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Control Theory

156 missions · 37 completed

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AnalysisPartial Differential Equations·Captain: mikedeng1

Stability and Instability Results of the Wave Equation with a Delay Term in the Boundary or Internal Feedbacks I: Exponential Decay under Delayed Boundary FeedbackResearch Paper

Motivation

Boundary feedback stabilization of the wave equation asks whether a vibrating body at rest on part of its boundary can be brought to rest by a damping law on the rest of its boundary. With the undelayed velocity feedback ∂u/∂ν=−μ1ut\partial u/\partial\nu = -\mu_1 u_t∂u/∂ν=−μ1​ut​, the energy decays exponentially under geometric conditions on the domain; results of this kind go back to Chen (1979, 1981), Lagnese (1983, 1988), Lasiecka and Triggiani (1987), and Komornik and Zuazua (1990).

Real controllers act with a delay, and delays can destroy stability. Datko, Lagnese and Polis (1986) and Datko (1988) showed that an arbitrarily small delay in a boundary feedback that stabilizes the one-dimensional wave equation can make the closed loop unstable. For a feedback made of an undelayed part and a delayed part, μ1ut(t)+μ2ut(t−τ)\mu_1 u_t(t) + \mu_2 u_t(t-\tau)μ1​ut​(t)+μ2​ut​(t−τ), Xu, Yung and Li (2006) proved, by spectral analysis in one space dimension, that the system is stable when μ2<μ1\mu_2 < \mu_1μ2​<μ1​. Nicaise and Pignotti (2006) extended the stability result to bounded domains in any dimension nnn. This mission formalizes that extension: Theorem 1.1 of their paper.

Setting

Let Ω⊂Rn\Omega \subset \mathbb R^nΩ⊂Rn (n≥1n \ge 1n≥1) be a bounded open set whose boundary Γ\GammaΓ is of class C2C^2C2. The boundary is split as Γ=ΓD∪ΓN\Gamma = \Gamma_D \cup \Gamma_NΓ=ΓD​∪ΓN​, with ΓD‾∩ΓN‾=∅\overline{\Gamma_D} \cap \overline{\Gamma_N} = \emptysetΓD​​∩ΓN​​=∅ and ΓD≠∅\Gamma_D \ne \emptysetΓD​=∅. Let ν\nuν be the outer unit normal and dΓd\GammadΓ the surface measure on Γ\GammaΓ. Fix the undelayed gain μ1>0\mu_1 > 0μ1​>0, the delayed gain μ2>0\mu_2 > 0μ2​>0 and the delay τ>0\tau > 0τ>0. The problem is

utt−Δu=0in Ω×(0,∞),(1.1)u=0on ΓD×(0,∞),(1.2)∂u∂ν(x,t)=−μ1ut(x,t)−μ2ut(x,t−τ)on ΓN×(0,∞),(1.3)\begin{aligned} u_{tt} - \Delta u &= 0 && \text{in } \Omega \times (0,\infty), &(1.1)\\ u &= 0 && \text{on } \Gamma_D \times (0,\infty), &(1.2)\\ \tfrac{\partial u}{\partial \nu}(x,t) &= -\mu_1 u_t(x,t) - \mu_2 u_t(x,t-\tau) && \text{on } \Gamma_N \times (0,\infty), &(1.3) \end{aligned}utt​−Δuu∂ν∂u​(x,t)​=0=0=−μ1​ut​(x,t)−μ2​ut​(x,t−τ)​​in Ω×(0,∞),on ΓD​×(0,∞),on ΓN​×(0,∞),​(1.1)(1.2)(1.3)​

with initial data u(⋅,0)=u0u(\cdot,0) = u_0u(⋅,0)=u0​ and ut(⋅,0)=u1u_t(\cdot,0) = u_1ut​(⋅,0)=u1​ in Ω\OmegaΩ, and a history ut=f0u_t = f_0ut​=f0​ on ΓN×(−τ,0)\Gamma_N \times (-\tau, 0)ΓN​×(−τ,0) (1.4)–(1.5).

The geometric hypothesis requires a function v∈C2(Ω‾)v \in C^2(\overline\Omega)v∈C2(Ω) and a constant α>0\alpha > 0α>0 with two properties:

⟨D2v(x)ξ,ξ⟩≥2α∣ξ∣2(x∈Ω‾, ξ∈Rn),(1.6)\langle D^2 v(x)\xi,\xi\rangle \ge 2\alpha|\xi|^2 \quad (x \in \overline\Omega,\ \xi \in \mathbb R^n), \tag{1.6}⟨D2v(x)ξ,ξ⟩≥2α∣ξ∣2(x∈Ω, ξ∈Rn),(1.6) ∇v(x)⋅ν(x)≤0(x∈ΓD).(1.7)\nabla v(x)\cdot\nu(x) \le 0 \quad (x \in \Gamma_D). \tag{1.7}∇v(x)⋅ν(x)≤0(x∈ΓD​).(1.7)

For example, v(x)=∣x∣2v(x) = |x|^2v(x)=∣x∣2 satisfies both on an annulus whose inner sphere is ΓD\Gamma_DΓD​.

Assume the gain condition

μ2<μ1,(1.8)\mu_2 < \mu_1, \tag{1.8}μ2​<μ1​,(1.8)

and fix ξ\xiξ with

τμ2<ξ<τ(2μ1−μ2).(1.10)\tau\mu_2 < \xi < \tau(2\mu_1 - \mu_2). \tag{1.10}τμ2​<ξ<τ(2μ1​−μ2​).(1.10)

The energy of a solution is the standard wave energy plus a term that stores the delayed velocity:

E(t)=12∫Ω{ut2(x,t)+∣∇u(x,t)∣2} dx+ξ2∫ΓN∫01ut2(x,t−τρ) dρ dΓ.(1.9)E(t) = \frac12\int_\Omega \{u_t^2(x,t) + |\nabla u(x,t)|^2\}\,dx + \frac{\xi}{2}\int_{\Gamma_N}\int_0^1 u_t^2(x,t-\tau\rho)\,d\rho\,d\Gamma. \tag{1.9}E(t)=21​∫Ω​{ut2​(x,t)+∣∇u(x,t)∣2}dx+2ξ​∫ΓN​​∫01​ut2​(x,t−τρ)dρdΓ.(1.9)

Formalization targets

Goal: Theorem 1.1 (exponential decay)

There are constants C1,C2>0C_1, C_2 > 0C1​,C2​>0, depending on Ω,ΓD,ΓN,v,α,μ1,μ2,τ,ξ\Omega, \Gamma_D, \Gamma_N, v, \alpha, \mu_1, \mu_2, \tau, \xiΩ,ΓD​,ΓN​,v,α,μ1​,μ2​,τ,ξ but not on the solution, such that every regular solution satisfies

E(t)≤C1E(0) e−C2t∀t≥0.(1.11)E(t) \le C_1 E(0)\, e^{-C_2 t} \qquad \forall t \ge 0. \tag{1.11}E(t)≤C1​E(0)e−C2​t∀t≥0.(1.11)

The constants are existential and are not fixed numerically. Any valid pair proves the goal.

Milestones, in the order the paper's proof uses them

  1. (3.6): the energy identity, which expresses E′(t)E'(t)E′(t) through boundary integrals over ΓN\Gamma_NΓN​ only.
  2. Proposition 3.1: EEE is nonincreasing, and
E′(t)≤−C∫ΓN{ut2(x,t)+ut2(x,t−τ)} dΓ,C=min⁡{μ1−μ22−ξ2τ, −μ22+ξ2τ}>0.E'(t) \le -C\int_{\Gamma_N}\{u_t^2(x,t) + u_t^2(x,t-\tau)\}\,d\Gamma, \qquad C = \min\Big\{\mu_1 - \frac{\mu_2}{2} - \frac{\xi}{2\tau},\ -\frac{\mu_2}{2} + \frac{\xi}{2\tau}\Big\} > 0.E′(t)≤−C∫ΓN​​{ut2​(x,t)+ut2​(x,t−τ)}dΓ,C=min{μ1​−2μ2​​−2τξ​, −2μ2​​+2τξ​}>0.
  1. (3.22): the integrated form E(T)−E(0)≤−C∫0T∫ΓN{ut2(t)+ut2(t−τ)} dΓ dtE(T) - E(0) \le -C\int_0^T\int_{\Gamma_N}\{u_t^2(t) + u_t^2(t-\tau)\}\,d\Gamma\,dtE(T)−E(0)≤−C∫0T​∫ΓN​​{ut2​(t)+ut2​(t−τ)}dΓdt.
  2. Proposition 3.2 (observability): there is T‾>0\overline T > 0T>0 such that for every T>T‾T > \overline TT>T some C0>0C_0 > 0C0​>0 satisfies
E(0)≤C0∫0T∫ΓN{ut2(x,t)+ut2(x,t−τ)} dΓ dt.(3.10)E(0) \le C_0\int_0^T\int_{\Gamma_N}\{u_t^2(x,t) + u_t^2(x,t-\tau)\}\,d\Gamma\,dt. \tag{3.10}E(0)≤C0​∫0T​∫ΓN​​{ut2​(x,t)+ut2​(x,t−τ)}dΓdt.(3.10)
  1. Contraction: there are T>0T > 0T>0 and 0≤C~<10 \le \tilde C < 10≤C~<1 with E(T)≤C~E(0)E(T) \le \tilde C E(0)E(T)≤C~E(0) for every regular solution.

Significance

The theorem shows that adding a delayed component to a stabilizing boundary feedback preserves exponential decay if the delayed gain is dominated by the undelayed gain. It holds in every dimension, under the same geometric condition that governs the undelayed problem. The companion Theorem 1.2 of the same paper shows that the condition μ2<μ1\mu_2 < \mu_1μ2​<μ1​ cannot be removed: when it fails, there are delays for which some solutions keep constant, positive standard energy. The Lyapunov functional (1.9) became a standard device for delayed feedbacks in later work on wave, plate and Timoshenko systems.

The result was proved in 2006. It has no machine-checked proof. This mission produces:

  • a formal statement of the theorem on classical solutions;
  • the energy identity and dissipation inequality with explicit constants;
  • the observability inequality as a separate target, which is the deep analytic input and is reusable by any stabilization argument on the same geometry.

Difficulty

The dissipation inequality (Proposition 3.1) is a calculation: Green's formula, a change of variables in the delay variable ρ\rhoρ, and Young's inequality. The difficulty is entirely in the observability inequality (3.10). The obvious multiplier argument, which multiplies the equation by ∇v⋅∇u\nabla v\cdot\nabla u∇v⋅∇u and integrates, leaves a lower-order term ∥u∥\|u\|∥u∥ that the boundary observation does not control.

The paper removes that term in two steps. The first is a Carleman-type estimate of Lasiecka, Triggiani and Yao (1999), which is where hypotheses (1.6)–(1.7) enter. The second is a compactness–uniqueness argument closed by Holmgren's uniqueness theorem. None of these tools exists in Mathlib, and neither does Green's formula on a curved domain. The final step from a one-period contraction to exponential decay uses time-translation invariance and monotonicity of EEE.

Formalization scope

  • Domain. A MixedDomain n bundles the following:

    • a bounded open set given by a global C2C^2C2 defining function ψ\psiψ (Ω={ψ<0}\Omega = \{\psi < 0\}Ω={ψ<0}, ∂Ω={ψ=0}\partial\Omega = \{\psi = 0\}∂Ω={ψ=0}, ∇ψ≠0\nabla\psi \ne 0∇ψ=0 on ∂Ω\partial\Omega∂Ω);
    • the split ΓD∪ΓN=∂Ω\Gamma_D \cup \Gamma_N = \partial\OmegaΓD​∪ΓN​=∂Ω with disjoint closures and ΓD≠∅\Gamma_D \ne \emptysetΓD​=∅;
    • a finite measure σ\sigmaσ carried by ∂Ω\partial\Omega∂Ω satisfying the Gauss–Green formula for every C1C^1C1 vector field.

    The outer normal is ν=∇ψ/∣∇ψ∣\nu = \nabla\psi/|\nabla\psi|ν=∇ψ/∣∇ψ∣. The Gauss–Green requirement determines σ\sigmaσ uniquely as the surface measure, so the normalization of dΓd\GammadΓ in (1.9) and (1.10) is the paper's.

  • Solutions are real-valued and classical: uuu is one C2C^2C2 function on Rn×R\mathbb R^n \times \mathbb RRn×R. It satisfies (1.1)–(1.3) for t>0t > 0t>0, and its values at t≤0t \le 0t≤0 are the initial data and the history. Time derivatives are one-variable derivatives in ttt, and ∂u/∂ν=∇u⋅ν\partial u/\partial\nu = \nabla u \cdot \nu∂u/∂ν=∇u⋅ν. This is a subclass of the paper's solutions, so the formal theorems are the paper's restricted to smooth, compatible data.

  • Added hypothesis. In Proposition 3.2, the contraction step and the goal, every connected component of Ω\OmegaΩ has a boundary point in ΓD\Gamma_DΓD​ (true whenever Ω\OmegaΩ is connected). The paper's uniqueness step ("−Δw=0-\Delta w = 0−Δw=0, w=0w = 0w=0 on ΓD\Gamma_DΓD​, ∂w/∂ν=0\partial w/\partial\nu = 0∂w/∂ν=0 on ΓN\Gamma_NΓN​, so w≡0w \equiv 0w≡0") needs every component of Ω\OmegaΩ to meet ΓD\Gamma_DΓD​.

  • Strengthened statements. The identity (3.6) and Propositions 3.1 and (3.22) omit hypotheses they do not use. Proposition 3.1 states the explicit constant CCC from the end of its proof.

  • Conventions. Condition (1.10) is strict. The energy is EEE of (1.9), with the delay term, and not the standard energy. Derivatives of EEE are asserted with HasDerivAt.

  • Excluded trivializations. Three things would make the statements empty or different, and none of them is allowed:

    • a free measure in place of the surface measure;
    • the standard energy in place of EEE;
    • replacing (1.11) by E(t)→0E(t) \to 0E(t)→0.

    The degenerate case ΓN=∅\Gamma_N = \emptysetΓN​=∅ is already excluded by (1.6), (1.7) and Gauss–Green together.

  • Infrastructure needed and welcome:

    • Gauss–Green and Green's first identity on MixedDomain;
    • differentiation under the integral over Ω\OmegaΩ and ΓN\Gamma_NΓN​;
    • a Carleman or multiplier observability estimate for the wave equation with mixed boundary conditions;
    • unique continuation (Holmgren) for the wave equation;
    • the elementary lemma turning a one-period contraction plus monotonicity into exponential decay.

    The last lemma and Gauss–Green on C2C^2C2 domains are reusable far beyond this mission.

Selected references

  • S. Nicaise, C. Pignotti, Stability and instability results of the wave equation with a delay term in the boundary or internal feedbacks, SIAM J. Control Optim. 45(5) (2006), 1561–1585. https://doi.org/10.1137/060648891
  • G. Q. Xu, S. P. Yung, L. K. Li, Stabilization of wave systems with input delay in the boundary control, ESAIM Control Optim. Calc. Var. 12 (2006), 770–785. https://doi.org/10.1051/cocv:2006021
  • R. Datko, J. Lagnese, M. P. Polis, An example on the effect of time delays in boundary feedback stabilization of wave equations, SIAM J. Control Optim. 24 (1986), 152–156. https://doi.org/10.1137/0324007
  • R. Datko, Not all feedback stabilized hyperbolic systems are robust with respect to small time delays in their feedbacks, SIAM J. Control Optim. 26 (1988), 697–713. https://doi.org/10.1137/0326040
  • I. Lasiecka, R. Triggiani, P. F. Yao, Inverse/observability estimates for second-order hyperbolic equations with variable coefficients, J. Math. Anal. Appl. 235 (1999), 13–57. https://doi.org/10.1006/jmaa.1999.6348
  • V. Komornik, E. Zuazua, A direct method for the boundary stabilization of the wave equation, J. Math. Pures Appl. 69 (1990), 33–54.
  • J. Lagnese, Decay of solutions of wave equations in a bounded region with boundary dissipation, J. Differential Equations 50 (1983), 163–182. https://doi.org/10.1016/0022-0396(83)90073-6
9 thms1 active userReviewed
AnalysisDynamical Systems·Captain: mikedeng1

Stabilization for a Perturbed Chain of Integrators in Prescribed Time II: Fixed-Time and Prescribed-Time Stability of the Varying-Degree Homogeneous FeedbackResearch Paper

Motivation

Many control tasks come with a deadline: a consensus protocol or a regulation task must reach its target by a time fixed in advance, whatever the initial condition. Prescribed-time stabilization asks for a feedback law that brings every trajectory of a control system to the equilibrium by a user-chosen time TTT. The basic test case is the chain of integrators x1(n)=ux_1^{(n)}=ux1(n)​=u, the normal form of every single-input feedback-linearizable system.

Two routes to prescribed-time stabilization exist. Time-varying gains that blow up as t→Tt\to Tt→T (Song, Wang, Holloway and Krstić, Automatica 2017) are fragile under measurement noise. Fixed-time stabilization gives a settling time bounded uniformly over all initial conditions, and a time rescaling then turns the uniform bound into any prescribed TTT. Chitour, Ushirobira and Bouhemou (SIAM J. Control Optim. 2020) follow the second route with an explicit, continuous feedback. It combines Hong's backstepping homogeneous controller (Systems Control Lett. 2002) with a degree of homogeneity that depends on the state (Harmouche, Laghrouche, Chitour and Hamerlain, Int. J. Control 2017). A continuity device of Lopez-Ramirez, Efimov, Polyakov and Perruquetti (Int. J. Robust Nonlinear Control 2018) makes that degree a continuous function of the state. This mission formalizes the construction and its main results, §4.1–4.2 of the paper.

Setting

Fix n≥1n\ge1n≥1 and write x=(x1,…,xn)∈Rnx=(x_1,\dots,x_n)\in\mathbb R^nx=(x1​,…,xn​)∈Rn with the Euclidean norm. Let JnJ_nJn​ be the nnn-th Jordan block (Jnei=ei−1J_ne_i=e_{i-1}Jn​ei​=ei−1​, e0=0e_0=0e0​=0). The pure chain of integrators (31) is

x˙=Jnx+u en.\dot x=J_nx+u\,e_n .x˙=Jn​x+uen​.

For y∈Ry\in\mathbb Ry∈R and a>0a>0a>0 write ⌈y⌋a=sign⁡(y)∣y∣a\lceil y\rfloor^a=\operatorname{sign}(y)|y|^a⌈y⌋a=sign(y)∣y∣a. Given gains ℓ1,…,ℓn>0\ell_1,\dots,\ell_n>0ℓ1​,…,ℓn​>0 and κ∈[−12n,12n]\kappa\in[-\tfrac1{2n},\tfrac1{2n}]κ∈[−2n1​,2n1​], set rj=1+(j−1)κr_j=1+(j-1)\kapparj​=1+(j−1)κ and βj=(2+κ)/rj+1−1\beta_j=(2+\kappa)/r_{j+1}-1βj​=(2+κ)/rj+1​−1. Define v0=0v_0=0v0​=0 and

vj=−ℓj⌈⌈xj⌋βj−1−⌈vj−1⌋βj−1⌋rj+κrjβj−1.v_j=-\ell_j\Big\lceil\lceil x_j\rfloor^{\beta_{j-1}}-\lceil v_{j-1}\rfloor^{\beta_{j-1}}\Big\rfloor^{\frac{r_j+\kappa}{r_j\beta_{j-1}}} .vj​=−ℓj​⌈⌈xj​⌋βj−1​−⌈vj−1​⌋βj−1​⌋rj​βj−1​rj​+κ​.

The homogeneous feedback is ωκH(x)=vn(x)\omega^H_\kappa(x)=v_n(x)ωκH​(x)=vn​(x) (Definition 23). The associated Lyapunov function is

Vκ(x)=∑j=1n∣xj∣βj−1+1−∣vj−1∣βj−1+1βj−1+1−⌈vj−1⌋βj−1(xj−vj−1),V_\kappa(x)=\sum_{j=1}^n\frac{|x_j|^{\beta_{j-1}+1}-|v_{j-1}|^{\beta_{j-1}+1}}{\beta_{j-1}+1}-\lceil v_{j-1}\rfloor^{\beta_{j-1}}(x_j-v_{j-1}),Vκ​(x)=j=1∑n​βj−1​+1∣xj​∣βj−1​+1−∣vj−1​∣βj−1​+1​−⌈vj−1​⌋βj−1​(xj​−vj−1​),

and (36) is the decay inequality V˙κ≤−CVκ1+α(κ)\dot V_\kappa\le-CV_\kappa^{1+\alpha(\kappa)}V˙κ​≤−CVκ1+α(κ)​, with α(κ)=κ/(2+κ)\alpha(\kappa)=\kappa/(2+\kappa)α(κ)=κ/(2+κ) and one constant CCC for all κ\kappaκ in the range.

For m∈(0,1)m\in(0,1)m∈(0,1) and κ0∈(0,12n)\kappa_0\in(0,\tfrac1{2n})κ0​∈(0,2n1​), the state-dependent degree κ(x)\kappa(x)κ(x) of (49) equals κ0\kappa_0κ0​ where V0(x)>1+mV_0(x)>1+mV0​(x)>1+m and −κ0-\kappa_0−κ0​ where V0(x)<1−mV_0(x)<1-mV0​(x)<1−m, and it interpolates linearly in V0V_0V0​ in between. The closed-loop controller is ωκ(x)H(x)\omega^H_{\kappa(x)}(x)ωκ(x)H​(x). With B<aκ={Vκ<a}B^\kappa_{<a}=\{V_\kappa<a\}B<aκ​={Vκ​<a}, let r(m,κ0)r(m,\kappa_0)r(m,κ0​) be the largest rrr with B<rκ0⊆B<1+m0B^{\kappa_0}_{<r}\subseteq B^0_{<1+m}B<rκ0​​⊆B<1+m0​, and r(m,−κ0)r(m,-\kappa_0)r(m,−κ0​) the smallest rrr with B<r−κ0⊇B<1−m0B^{-\kappa_0}_{<r}\supseteq B^0_{<1-m}B<r−κ0​​⊇B<1−m0​. Set

T∗(m,κ0)=1C(r(m,κ0)−α(κ0)α(κ0)−2ln⁡(2m)+r(m,−κ0)−α(−κ0)−α(−κ0)).T^\ast(m,\kappa_0)=\frac1C\Big(\frac{r(m,\kappa_0)^{-\alpha(\kappa_0)}}{\alpha(\kappa_0)}-2\ln(2m)+\frac{r(m,-\kappa_0)^{-\alpha(-\kappa_0)}}{-\alpha(-\kappa_0)}\Big).T∗(m,κ0​)=C1​(α(κ0​)r(m,κ0​)−α(κ0​)​−2ln(2m)+−α(−κ0​)r(m,−κ0​)−α(−κ0​)​).

Finally Dλr=diag⁡(λn−i+1)D^{\mathbf r}_\lambda=\operatorname{diag}(\lambda^{n-i+1})Dλr​=diag(λn−i+1) is the dilation of (5).

A system is globally fixed-time stable with settling time at most TTT if the origin is an equilibrium, solutions exist from every initial state, it is Lyapunov stable, and every solution vanishes for all t≥Tt\ge Tt≥T (Definition 1 with Ω=Rn\Omega=\mathbb R^nΩ=Rn).

Formalization targets

Goal: Theorem 30 (p. 1038)

Let the gains and C>0C>0C>0 satisfy (36). There are m∈(0,1)m\in(0,1)m∈(0,1) and κ0∈(0,12n)\kappa_0\in(0,\tfrac1{2n})κ0​∈(0,2n1​) such that, for every T>0T>0T>0 and every λ>0\lambda>0λ>0 with

λ ≥ T∗(m,κ0)/T,\lambda\ \ge\ T^\ast(m,\kappa_0)/T,λ ≥ T∗(m,κ0​)/T,

the feedback u=ωκ(Dλrx)H(Dλrx)u=\omega^H_{\kappa(D^{\mathbf r}_\lambda x)}(D^{\mathbf r}_\lambda x)u=ωκ(Dλr​x)H​(Dλr​x) makes (31) globally fixed-time stable with settling time at most TTT.

Milestones

  • Proposition 24 (p. 1034): gains exist for which (36) holds uniformly in κ\kappaκ, VκV_\kappaVκ​ is C1C^1C1, positive definite and r(κ)\mathbf r(\kappa)r(κ)-homogeneous of degree 2+κ2+\kappa2+κ, and ωκH\omega^H_\kappaωκH​ is globally asymptotically stabilizing.
  • Lemma 31 (p. 1038): on the shell B1−m,1+mκB^\kappa_{1-m,1+m}B1−m,1+mκ​, ∣xj∣|x_j|∣xj​∣ and ∣vj∣|v_j|∣vj​∣ are bounded uniformly in κ\kappaκ.
  • Lemma 32 (p. 1039): on that shell, ∣ωκH−ω0H∣|\omega^H_\kappa-\omega^H_0|∣ωκH​−ω0H​∣ and ∣Vκ−V0∣|V_\kappa-V_0|∣Vκ​−V0​∣ are at most a constant times ∣κ∣min⁡(1,rn)|\kappa|^{\min(1,r_n)}∣κ∣min(1,rn​).
  • Proposition 33 (p. 1040): for every mmm there is κ0(m)>0\kappa_0(m)>0κ0​(m)>0 below which the closed loop is fixed-time stable, with an explicit settling-time bound that coincides with (52) for m≤(17−3)/4m\le(\sqrt{17}-3)/4m≤(17​−3)/4.
  • Theorem 28 (pp. 1036–1037): with an input gain b(t)∈[b‾,bˉ]b(t)\in[\underline b,\bar b]b(t)∈[b​,bˉ] and the feedback ωκ(x)H(x)/b‾\omega^H_{\kappa(x)}(x)/\underline bωκ(x)H​(x)/b​, the closed loop is globally fixed-time stable with settling time at most T∗(m,κ0)T^\ast(m,\kappa_0)T∗(m,κ0​).

Significance

The result gives a static, continuous state feedback for the chain of integrators with an explicit settling-time bound. It is robust to a bounded uncertain input gain, and the rescaled controller meets any prescribed deadline. Unlike time-varying designs, the gains stay bounded, which is what the paper's ISS analysis in §4.3 builds on. The constants in (52) are explicit in terms of CCC and the radii r(m,±κ0)r(m,\pm\kappa_0)r(m,±κ0​), so the rescaling factor λ\lambdaλ is computable.

The results are proved on paper; no machine-checked proof is known. A formalization would check the parameter bookkeeping of the construction: index shifts, exponents, the three-phase settling-time estimate, and the interplay of two different dilations. It would also produce reusable definitions of Carathéodory solutions and of finite-, fixed- and prescribed-time stability, which the platform does not yet have.

Difficulty

The obvious argument uses the Lyapunov function Vκ(x)V_{\kappa(x)}Vκ(x)​ for the varying-degree controller. That fails: κ\kappaκ depends on xxx, so Vκ(x)(x)V_{\kappa(x)}(x)Vκ(x)​(x) acquires a term from the derivative of κ\kappaκ. The proof instead handles three regions separately, with Vκ0V_{\kappa_0}Vκ0​​ outside B1+m0B^0_{1+m}B1+m0​, V0V_0V0​ on the shell B1−m,1+m0B^0_{1-m,1+m}B1−m,1+m0​, and V−κ0V_{-\kappa_0}V−κ0​​ inside B1−m0B^0_{1-m}B1−m0​. On the shell the controller is a perturbation of the linear one, and bounding that perturbation needs uniform Hölder estimates in κ\kappaκ (Lemmas 31–32). The closed loop is only continuous, so solutions need not be unique and every stability claim is about all solutions. Proposition 24 itself is a recursive gain construction whose constants must be uniform in κ\kappaκ.

Formalization scope

States are EuclideanSpace ℝ (Fin n); the paper's index j∈{1,…,n}j\in\{1,\dots,n\}j∈{1,…,n} is j.val + 1. Solutions are Carathéodory solutions on [0,∞)[0,\infty)[0,∞) in integral form, with integrability stated. Every stability property quantifies over all solutions, and existence of a solution from each initial state is part of Lyapunov stability. ⌈y⌋a\lceil y\rfloor^a⌈y⌋a is read as sign⁡(y)∣y∣a\operatorname{sign}(y)|y|^asign(y)∣y∣a; the paper never defines it. V˙\dot VV˙ is the Fréchet derivative applied to the vector field. r(m,κ0)r(m,\kappa_0)r(m,κ0​) and r(m,−κ0)r(m,-\kappa_0)r(m,−κ0​) are the supremum and infimum of the admissible radii.

Hypotheses and readings that differ from the page:

  • The gains and CCC in Theorems 28 and 30 and Proposition 33 are data satisfying (36), not existentially chosen. An unconstrained ∃C\exists C∃C would make (52) false, and Proposition 24 shows (36) is satisfiable.
  • bbb is assumed measurable in Theorem 28.
  • "Adapted" is the feedback divided by b‾\underline bb​, as the page says.
  • Corrected printed slips:
    • (51) lacks ene_nen​.
    • Theorem 30 writes κ0∈(0,1/n)\kappa_0\in(0,1/n)κ0​∈(0,1/n); Theorem 28's (0,12n)(0,\tfrac1{2n})(0,2n1​) is used.
    • Proposition 33 prints κ0(m)∈[−12n,−12n]\kappa_0(m)\in[-\tfrac1{2n},-\tfrac1{2n}]κ0​(m)∈[−2n1​,−2n1​]; the value is positive and at most 12n\tfrac1{2n}2n1​.
    • (37) prints βi−1\beta_{i-1}βi−1​ for βj−1\beta_{j-1}βj−1​.
    • The proof of Lemma 32 prints the exponent of (33) as (rj+1)/(rjβj−1)(r_j+1)/(r_j\beta_{j-1})(rj​+1)/(rj​βj−1​); (33) is used.
  • Lemma 32's maxima are read pointwise, with rn=rn(κ)r_n=r_n(\kappa)rn​=rn​(κ).
  • In Proposition 33 the middle term −2ln⁡(2m)-2\ln(2m)−2ln(2m) of (52) is replaced by max⁡(−2ln⁡(2m), 2ln⁡1+m1−m)\max(-2\ln(2m),\,2\ln\frac{1+m}{1-m})max(−2ln(2m),2ln1−m1+m​): the page's crossing-time estimate −2ln⁡(2m)/C-2\ln(2m)/C−2ln(2m)/C is justified only for m≤(17−3)/4m\le(\sqrt{17}-3)/4m≤(17​−3)/4, where the two bounds coincide.
  • "Explicit" constants are stated as existing.

A formalization in which (36) is dropped, or CCC is chosen freely, or a trajectory is only required to exist, would be trivial or false. Any trivializing reading of this kind is ruled out: stability is required of every solution, and CCC is tied to (36).

Needed infrastructure: signed powers and their Hölder estimates (42), differentiability of VκV_\kappaVκ​, weighted homogeneity, Carathéodory existence for continuous right-hand sides, and comparison lemmas for V˙≤−cV1+α\dot V\le-cV^{1+\alpha}V˙≤−cV1+α. The stability definitions and the comparison lemmas are reusable beyond this mission. Contributions of any of these are welcome.

Selected references

  • Y. Chitour, R. Ushirobira, H. Bouhemou, Stabilization for a Perturbed Chain of Integrators in Prescribed Time, SIAM J. Control Optim. 58(2), 1022–1048, 2020. https://doi.org/10.1137/19M1285937
  • Y. Hong, Finite-time stabilization and stabilizability of a class of controllable systems, Systems Control Lett. 46, 231–236, 2002. https://doi.org/10.1016/S0167-6911(02)00119-6
  • M. Harmouche, S. Laghrouche, Y. Chitour, M. Hamerlain, Stabilisation of perturbed chains of integrators using Lyapunov-based homogeneous controllers, Int. J. Control 90, 2631–2640, 2017. https://doi.org/10.1080/00207179.2016.1262967
  • F. Lopez-Ramirez, D. Efimov, A. Polyakov, W. Perruquetti, Fixed-time output stabilization and fixed-time estimation of a chain of integrators, Int. J. Robust Nonlinear Control 28, 4647–4665, 2018. https://doi.org/10.1002/rnc.4275
  • Y. Song, Y. Wang, J. Holloway, M. Krstić, Time-varying feedback for regulation of normal-form nonlinear systems in prescribed finite time, Automatica 83, 243–251, 2017. https://doi.org/10.1016/j.automatica.2017.06.008
  • S. P. Bhat, D. S. Bernstein, Geometric homogeneity with applications to finite-time stability, Math. Control Signals Systems 17, 101–127, 2005. https://doi.org/10.1007/s00498-005-0151-x
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Dynamical SystemsOperations ResearchProbability+1·Captain: mikedeng1

Stabilization of Hybrid Systems by Feedback Control Based on Discrete-Time State Observations II: Mean-Square and Almost Sure Exponential StabilityResearch Paper

Motivation

Many engineered systems switch between a finite number of operating modes at random times: a power grid after a line failure, a networked controller whose links drop, a manufacturing plant whose machines break down and are repaired. A standard model for such systems is a hybrid stochastic differential equation, also called an SDE with Markovian switching: the state follows an Itô equation whose coefficients depend on a mode that evolves as a continuous-time Markov chain. The monograph of Mao and Yuan (Stochastic Differential Equations with Markovian Switching, 2006) develops the stability theory of these equations.

A controller that stabilizes such a system usually needs the current state. In practice the state is sampled: it is observed at times 0,τ,2τ,…0,\tau,2\tau,\dots0,τ,2τ,… and the control is held between observations. Mao (Automatica 49, 2013) showed that, under a global Lipschitz condition on the drift and diffusion, a feedback control based on discrete-time observations makes a hybrid SDE mean-square exponentially stable when τ\tauτ is small enough. You, Liu, Lu, Mao and Qiu (SIAM J. Control Optim. 53(2), 2015) replaced that condition by local Lipschitz continuity plus linear growth, gave an explicit bound (3.5) on the admissible observation interval, and proved H∞H_\inftyH∞​-stability, asymptotic stability, and, in Section 4, exponential stability in mean square and almost surely with an explicit rate. This mission formalizes that exponential stability result, Theorem 4.2, and the steps of its proof.

Setting

Let (Ω,F,{Ft}t≥0,P)(\Omega,\mathcal F,\{\mathcal F_t\}_{t\ge0},\mathbb P)(Ω,F,{Ft​}t≥0​,P) be a probability space with a filtration satisfying the usual conditions (increasing, right-continuous, F0\mathcal F_0F0​ contains the null sets). On it live an mmm-dimensional {Ft}\{\mathcal F_t\}{Ft​}-Brownian motion www and a right-continuous {Ft}\{\mathcal F_t\}{Ft​}-Markov chain rrr on S={1,…,N}S=\{1,\dots,N\}S={1,…,N} with generator Γ=(γij)\Gamma=(\gamma_{ij})Γ=(γij​) (γij≥0\gamma_{ij}\ge0γij​≥0 for i≠ji\ne ji=j, zero row sums), independent of www. Fix τ>0\tau>0τ>0 and the sampling time δt=[t/τ]τ\delta_t=[t/\tau]\tauδt​=[t/τ]τ. The controlled system is

dx(t)=(f(x(t),r(t),t)+u(x(δt),r(t),t))dt+g(x(t),r(t),t) dw(t),x(0)=x0, r(0)=r0,(2.1)dx(t)=\big(f(x(t),r(t),t)+u(x(\delta_t),r(t),t)\big)dt+g(x(t),r(t),t)\,dw(t),\qquad x(0)=x_0,\ r(0)=r_0,\tag{2.1}dx(t)=(f(x(t),r(t),t)+u(x(δt​),r(t),t))dt+g(x(t),r(t),t)dw(t),x(0)=x0​, r(0)=r0​,(2.1)

with f,u:Rn×S×R+→Rnf,u:\mathbb R^n\times S\times\mathbb R_+\to\mathbb R^nf,u:Rn×S×R+​→Rn and g:Rn×S×R+→Rn×mg:\mathbb R^n\times S\times\mathbb R_+\to\mathbb R^{n\times m}g:Rn×S×R+​→Rn×m.

The hypotheses are:

  • Assumption 2.1: f,gf,gf,g locally Lipschitz in xxx, and ∣f(x,i,t)∣≤K1∣x∣|f(x,i,t)|\le K_1|x|∣f(x,i,t)∣≤K1​∣x∣, ∣g(x,i,t)∣≤K2∣x∣|g(x,i,t)|\le K_2|x|∣g(x,i,t)∣≤K2​∣x∣ (∣g∣|g|∣g∣ the trace norm).
  • Assumption 2.2: ∣u(x,i,t)−u(y,i,t)∣≤K3∣x−y∣|u(x,i,t)-u(y,i,t)|\le K_3|x-y|∣u(x,i,t)−u(y,i,t)∣≤K3​∣x−y∣ and u(0,i,t)=0u(0,i,t)=0u(0,i,t)=0.
  • Assumption 3.1: there are U∈C2,1(Rn×S×R+;R+)U\in C^{2,1}(\mathbb R^n\times S\times\mathbb R_+;\mathbb R_+)U∈C2,1(Rn×S×R+​;R+​) and λ1,λ2>0\lambda_1,\lambda_2>0λ1​,λ2​>0 with LU(x,i,t)+λ1∣Ux(x,i,t)∣2≤−λ2∣x∣2\mathcal LU(x,i,t)+\lambda_1|U_x(x,i,t)|^2\le-\lambda_2|x|^2LU(x,i,t)+λ1​∣Ux​(x,i,t)∣2≤−λ2​∣x∣2, where
LU=Ut+Ux[f+u]+12trace⁡[gTUxxg]+∑jγijU(x,j,t).\mathcal LU=U_t+U_x[f+u]+\tfrac12\operatorname{trace}[g^TU_{xx}g]+\sum_j\gamma_{ij}U(x,j,t).LU=Ut​+Ux​[f+u]+21​trace[gTUxx​g]+j∑​γij​U(x,j,t).
  • Assumption 4.1: c1∣x∣2≤U(x,i,t)≤c2∣x∣2c_1|x|^2\le U(x,i,t)\le c_2|x|^2c1​∣x∣2≤U(x,i,t)≤c2​∣x∣2 with c1,c2>0c_1,c_2>0c1​,c2​>0.
  • Condition (3.5): λ2>τK32λ1[2τ(K12+2K32)+K22]\lambda_2>\frac{\tau K_3^2}{\lambda_1}\big[2\tau(K_1^2+2K_3^2)+K_2^2\big]λ2​>λ1​τK32​​[2τ(K12​+2K32​)+K22​] and τ≤14K3\tau\le\frac1{4K_3}τ≤4K3​1​.

Put θ=K32/λ1\theta=K_3^2/\lambda_1θ=K32​/λ1​, λ=λ2−θτ[2τ(K12+2K32)+K22]\lambda=\lambda_2-\theta\tau[2\tau(K_1^2+2K_3^2)+K_2^2]λ=λ2​−θτ[2τ(K12​+2K32​)+K22​] (positive by (3.5)), and

H1=θτ(2τ(K12+2K32)+K22)+24θτ4K341−6τ2K32,H2=12θτ2K32(τK12+K22)1−6τ2K32.H_1=\theta\tau\big(2\tau(K_1^2+2K_3^2)+K_2^2\big)+\frac{24\theta\tau^4K_3^4}{1-6\tau^2K_3^2},\qquad H_2=\frac{12\theta\tau^2K_3^2(\tau K_1^2+K_2^2)}{1-6\tau^2K_3^2}.H1​=θτ(2τ(K12​+2K32​)+K22​)+1−6τ2K32​24θτ4K34​​,H2​=1−6τ2K32​12θτ2K32​(τK12​+K22​)​.

In Lean these are Assumption21, Assumption22, C21, LU, Assumption31, Assumption41, Condition35, theta, lam, H1, H2, rateEquationLHS; the basis is HybridSetup, the Itô integral IsItoIntegral, the sampling time delta, solutions SolvesSampledHybridSDE, and the functional (4.7) Vbar, all in the namespace You2015.Expo.

Formalization targets

Goal: Theorem 4.2 (exponential stability)

Under the hypotheses above, the equation

2τγe2τγ(H1+τH2)+γc2=λ(4.4)2\tau\gamma e^{2\tau\gamma}(H_1+\tau H_2)+\gamma c_2=\lambda\tag{4.4}2τγe2τγ(H1​+τH2​)+γc2​=λ(4.4)

has a unique root γ>0\gamma>0γ>0, and every solution of (2.1) satisfies

lim sup⁡t→∞1tlog⁡(E∣x(t)∣2)≤−γ,lim sup⁡t→∞1tlog⁡∣x(t)∣≤−γ2a.s.\limsup_{t\to\infty}\frac1t\log\big(\mathbb E|x(t)|^2\big)\le-\gamma,\qquad\limsup_{t\to\infty}\frac1t\log|x(t)|\le-\frac\gamma2\quad\text{a.s.}t→∞limsup​t1​log(E∣x(t)∣2)≤−γ,t→∞limsup​t1​log∣x(t)∣≤−2γ​a.s.

for all x0∈Rnx_0\in\mathbb R^nx0​∈Rn, r0∈Sr_0\in Sr0​∈S.

Milestones, in the order the proof uses them

  1. (3.15) E∣x(t)−x(δt)∣2≤2E∫δtt[τ∣f+u(x(δs),⋅)∣2+∣g∣2]ds\mathbb E|x(t)-x(\delta_t)|^2\le2\mathbb E\int_{\delta_t}^t[\tau|f+u(x(\delta_s),\cdot)|^2+|g|^2]dsE∣x(t)−x(δt​)∣2≤2E∫δt​t​[τ∣f+u(x(δs​),⋅)∣2+∣g∣2]ds.
  2. Theorem 3.2 (H∞H_\inftyH∞​-stability): ∫0∞E∣x(s)∣2ds<∞\int_0^\infty\mathbb E|x(s)|^2ds<\infty∫0∞​E∣x(s)∣2ds<∞.
  3. (3.21) E∣x(s)−x(δs)∣2≤3(τK12+K22)1−6τ2K32∫δssE∣x(z)∣2dz+6τ2K321−6τ2K32E∣x(s)∣2\mathbb E|x(s)-x(\delta_s)|^2\le\frac{3(\tau K_1^2+K_2^2)}{1-6\tau^2K_3^2}\int_{\delta_s}^s\mathbb E|x(z)|^2dz+\frac{6\tau^2K_3^2}{1-6\tau^2K_3^2}\mathbb E|x(s)|^2E∣x(s)−x(δs​)∣2≤1−6τ2K32​3(τK12​+K22​)​∫δs​s​E∣x(z)∣2dz+1−6τ2K32​6τ2K32​​E∣x(s)∣2.
  4. (4.11) EVˉ(x^z,r^z,z)≤(H1+τH2)∫z−2τzE∣x(y)∣2dy\mathbb E\bar V(\hat x_z,\hat r_z,z)\le(H_1+\tau H_2)\int_{z-2\tau}^z\mathbb E|x(y)|^2dyEVˉ(x^z​,r^z​,z)≤(H1​+τH2​)∫z−2τz​E∣x(y)∣2dy for z≥2τz\ge2\tauz≥2τ.
  5. (4.14) c1eγtE∣x(t)∣2≤Cc_1e^{\gamma t}\mathbb E|x(t)|^2\le Cc1​eγtE∣x(t)∣2≤C for t≥2τt\ge2\taut≥2τ.
  6. (4.14) ⇒\Rightarrow⇒ (4.3), the mean-square-to-almost-sure transfer cited from Mao–Yuan [23, Theorem 8.8].

Significance

The result. Theorem 4.2 gives a quantitative guarantee: a controller that samples the state every τ\tauτ units makes the switching system decay exponentially, with a rate γ\gammaγ computable from the constants of the assumptions. Asymptotic stability (Section 3 of the paper) says nothing about how fast trajectories settle; the rate is what a designer trades against the sampling cost when choosing τ\tauτ. The almost sure statement concerns individual trajectories, which is what an operator observes.

Formalizing it. The results are proved in the paper; none of them is machine-checked. Mathlib has real Brownian motion but no Itô integral, no stochastic differential equations and no continuous-time Markov chains. The mission therefore also produces a definition layer: a filtration under the usual conditions, a multidimensional {Ft}\{\mathcal F_t\}{Ft​}-Brownian motion, an {Ft}\{\mathcal F_t\}{Ft​}-Markov chain with a given generator, the L2L^2L2 Itô integral of vector-valued integrands, and the solution notion of an SDE with Markovian switching and a sampled-state delay. A related but different layer exists on Prove2Me for Ethier–Kurtz (EthierKurtz_IsStandardBrownian, EthierKurtz_HasBrownianItoIntegral, EthierKurtz_SolvesBrownianSDE); it has no mode switching and no sampled state, so it cannot express (2.1). Formalization also checks the constants: it found that the printed H1H_1H1​ in (4.5) disagrees with the paper's own derivation (see below).

Difficulty

Equation (2.1) is a stochastic differential delay equation whose delay t−δtt-\delta_tt−δt​ is bounded but jumps at every observation time, so the delay-equation stability theorems that require a differentiable delay with derivative below one (Mao–Yuan, p. 285) do not apply. A Lyapunov function of the current state alone leaves the term Ux[u(x(t))−u(x(δt))]U_x[u(x(t))-u(x(\delta_t))]Ux​[u(x(t))−u(x(δt​))], which has no sign and depends on the path over a whole observation interval. An exponential rate requires controlling this delay term with an exponential weight, and the weight inflates the delay contribution by a factor e2τγe^{2\tau\gamma}e2τγ; the rate equation (4.4) records exactly this balance. The almost sure part does not follow from the mean-square part by Chebyshev's inequality at fixed times alone: a pathwise bound needs control of the supremum of ∣x∣|x|∣x∣ over each unit interval, which involves the martingale part of the solution.

Formalization scope

Conventions committed to in Lean:

  • The state space is EuclideanSpace ℝ (Fin n), so ∣x∣|x|∣x∣ is the Euclidean norm; the explicit constants in (3.5), (3.21), (4.5) depend on it. The diffusion ggg is given by its mmm columns and ∣g∣2=∑k∣gk∣2|g|^2=\sum_k|g_k|^2∣g∣2=∑k​∣gk​∣2 (trace norm). Modes are Fin N (0-based). Time is ℝ≥0; time integrals are over subsets of R\mathbb RR at s.toNNReal.
  • Every expectation of a nonnegative quantity (E∣x∣2\mathbb E|x|^2E∣x∣2, EVˉ\mathbb E\bar VEVˉ) and every time integral of one is a lower Lebesgue integral in [0,∞][0,\infty][0,∞], so a non-integrable process cannot produce a junk value 000.
  • Logarithms. The paper's log⁡\loglog takes the value −∞-\infty−∞ at 000. For a finite a(t)≥0a(t)\ge0a(t)≥0, lim sup⁡t→∞1tlog⁡a(t)≤−γ\limsup_{t\to\infty}\frac1t\log a(t)\le-\gammalimsupt→∞​t1​loga(t)≤−γ is stated in the equivalent form "for every γ′<γ\gamma'<\gammaγ′<γ, eventually a(t)≤e−γ′ta(t)\le e^{-\gamma't}a(t)≤e−γ′t". Lean's Real.log 0 = 0 never enters. In (4.3) the almost-sure quantifier is outside the quantifier over γ′\gamma'γ′.
  • Correction of (4.5). The page prints the last term of H1H_1H1​ as 24τ3K34/(1−6τ2K32)24\tau^3K_3^4/(1-6\tau^2K_3^2)24τ3K34​/(1−6τ2K32​). Substituting (3.21) into (4.9), as the proof does, gives 24θτ4K34/(1−6τ2K32)24\theta\tau^4K_3^4/(1-6\tau^2K_3^2)24θτ4K34​/(1−6τ2K32​) (the same computation reproduces the printed H2H_2H2​). The mission uses the corrected H1H_1H1​ in the goal, (4.11) and (4.14). With the printed value the claimed rate could exceed what the proof yields whenever θτ>1\theta\tau>1θτ>1.
  • "The unique root" is a conjunct of the goal (∃! γ>0\exists!\,\gamma>0∃!γ>0); the stability conclusions are stated for every positive root. "(so λ>0\lambda>0λ>0)" is a consequence of (3.5), not a hypothesis. (4.4) is kept as an equality.
  • "The solution of (2.1)" is read as every process satisfying the solution definition: progressively measurable, almost surely continuous paths, E∣x(t)∣2<∞\mathbb E|x(t)|^2<\inftyE∣x(t)∣2<∞ for each ttt, and for each ttt, almost surely, the integral equation with Itô integrals in the L2L^2L2 sense. Existence and uniqueness (cited from Mao–Yuan on p. 908) are not asserted.
  • "An mmm-dimensional Brownian motion" and "a Markov chain with generator Γ\GammaΓ" are read in the Mao–Yuan framework the paper cites: an {Ft}\{\mathcal F_t\}{Ft​}-Brownian motion with independent coordinates and increments independent of the past, and an {Ft}\{\mathcal F_t\}{Ft​}-Markov chain with transition matrix etΓe^{t\Gamma}etΓ. The usual conditions are kept as hypotheses.
  • "Locally Lipschitz" is uniform in the mode and time on each ball. C2,1C^{2,1}C2,1 carries its derivatives Ut,Ux,UxxU_t,U_x,U_{xx}Ut​,Ux​,Uxx​ as witnesses tied to UUU by derivative relations and joint continuity.
  • "τ>0\tau>0τ>0 sufficiently small for (3.5)" means every τ>0\tau>0τ>0 satisfying both inequalities of (3.5). U,λ1,λ2,c1,c2,τU,\lambda_1,\lambda_2,c_1,c_2,\tauU,λ1​,λ2​,c1​,c2​,τ are data. The constant CCC of (4.14) is chosen after x0x_0x0​, r0r_0r0​, the solution and γ\gammaγ, and before ttt.
  • (3.15), (3.21) and the transfer (4.14) ⇒\Rightarrow⇒ (4.3) are stated under fewer hypotheses than the surrounding proof has (Assumptions 2.1, 2.2, τ>0\tau>0τ>0, and for (3.21) τ≤1/(4K3)\tau\le1/(4K_3)τ≤1/(4K3​)), because their derivations use no more. Vˉ\bar VVˉ of (4.7) is used only for z≥2τz\ge2\tauz≥2τ, where no extension of the solution to negative times is needed. Other misprints on the page (g(x,i,s)=f(x,i,0)g(x,i,s)=f(x,i,0)g(x,i,s)=f(x,i,0) on p. 909, V(x^0,r^0,t)V(\hat x_0,\hat r_0,t)V(x^0​,r^0​,t) for V(x^0,r^0,0)V(\hat x_0,\hat r_0,0)V(x^0​,r^0​,0) on p. 918, the swapped ∨,∧\vee,\wedge∨,∧ on p. 907) are not formalized.

A trivializing formalization is ruled out: the expectations are not Bochner integrals, log⁡0\log 0log0 is never evaluated, the goal asserts that the rate equation has exactly one positive root (so the stability clauses are not vacuous), the solution notion admits the true solution and requires path continuity, and the derivative witnesses of UUU are tied to UUU. A sorry-free local check confirms that Assumptions 2.1, 2.2, 4.1, condition (3.5) and λ>0\lambda>0λ>0 hold for n=m=N=1n=m=N=1n=m=N=1, f=g=0f=g=0f=g=0, u(x)=−xu(x)=-xu(x)=−x, U=∣x∣2U=|x|^2U=∣x∣2, K1=K2=K3=1K_1=K_2=K_3=1K1​=K2​=K3​=1, λ1=1/4\lambda_1=1/4λ1​=1/4, λ2=1\lambda_2=1λ2​=1, c1=c2=1c_1=c_2=1c1​=c2​=1, τ=1/10\tau=1/10τ=1/10; for these data LU+λ1∣Ux∣2=−∣x∣2\mathcal LU+\lambda_1|U_x|^2=-|x|^2LU+λ1​∣Ux​∣2=−∣x∣2 by hand.

Welcome contributions: the Itô isometry and Itô's formula for the L2L^2L2 integral defined here, a generalized Itô formula for functions of a Markov-modulated Itô process, the Burkholder–Davis–Gundy inequality, and the Borel–Cantelli argument that turns mean-square exponential decay into almost sure decay. These are reusable far beyond this mission. Section 3 of the paper (asymptotic stability) is a separate mission of the same series.

Selected references

  • S. You, W. Liu, J. Lu, X. Mao, Q. Qiu, Stabilization of Hybrid Systems by Feedback Control Based on Discrete-Time State Observations, SIAM J. Control Optim. 53(2), 905–925, 2015. https://doi.org/10.1137/140985779
  • X. Mao, C. Yuan, Stochastic Differential Equations with Markovian Switching, Imperial College Press, 2006. https://doi.org/10.1142/p473
  • X. Mao, Stabilization of continuous-time hybrid stochastic differential equations by discrete-time feedback control, Automatica 49(12), 3677–3681, 2013. https://doi.org/10.1016/j.automatica.2013.09.005
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Operations ResearchOptimization·Captain: mikedeng1

Optimizing Static Linear Feedback: Gradient Method II: The Gradient Flow Stays in the Sublevel Set and Converges Exponentially under State FeedbackResearch Paper

Motivation

The linear-quadratic regulator (LQR) is the basic problem of optimal control: steer a linear system x˙=Ax+Bu\dot x = Ax + Bux˙=Ax+Bu so as to minimize an integrated quadratic cost of state and input. When the full state is measured, the optimal law is a static linear feedback u=−Kxu = -Kxu=−Kx obtained from an algebraic Riccati equation. When only an output y=Cxy = Cxy=Cx is measured, the optimal static output feedback u=−Kyu = -Kyu=−Ky has no closed form, and the problem is nonconvex. In both cases the cost can be written as a function f(K)f(K)f(K) of the gain alone, which makes it natural to minimize fff by gradient methods directly in the space of gains. This view goes back to Levine and Athans (1970) for output feedback and was revived in reinforcement learning by Fazel, Ge, Kakade and Mesbahi (2018), who proved global convergence of policy gradient for discrete-time state-feedback LQR.

Fatkhullin and Polyak (arXiv:2004.09875v2, SIAM J. Control Optim. 2021) carry out this program for the continuous-time problem. They show that fff is coercive, that it is LLL-smooth on every sublevel set, and that under state feedback it satisfies a gradient-domination (Łojasiewicz–Polyak) inequality. From these properties they derive convergence of the continuous gradient flow and of the discrete gradient method. This mission formalizes the continuous part, Theorem 4.1.

Setting

Fix real matrices A∈Rn×nA\in\mathbb R^{n\times n}A∈Rn×n, B∈Rn×mB\in\mathbb R^{n\times m}B∈Rn×m, C∈Rr×nC\in\mathbb R^{r\times n}C∈Rr×n and symmetric positive definite weights Q∈Rn×nQ\in\mathbb R^{n\times n}Q∈Rn×n, R∈Rm×mR\in\mathbb R^{m\times m}R∈Rm×m and covariance Σ∈Rn×n\Sigma\in\mathbb R^{n\times n}Σ∈Rn×n. A gain is K∈Rm×rK\in\mathbb R^{m\times r}K∈Rm×r, and the closed-loop matrix is AK=A−BKCA_K = A - BKCAK​=A−BKC. A square matrix is Hurwitz if all its eigenvalues have negative real part. The stabilizing set is

S={K:AK is Hurwitz}.\mathcal S = \{K : A_K \text{ is Hurwitz}\}.S={K:AK​ is Hurwitz}.

For K∈SK\in\mathcal SK∈S, let X(K)X(K)X(K) and Y(K)Y(K)Y(K) be the unique solutions of the Lyapunov equations

AK⊤X+XAK+C⊤K⊤RKC+Q=0,AKY+YAK⊤+Σ=0.A_K^\top X + XA_K + C^\top K^\top RKC + Q = 0,\qquad A_KY + YA_K^\top + \Sigma = 0 .AK⊤​X+XAK​+C⊤K⊤RKC+Q=0,AK​Y+YAK⊤​+Σ=0.

The LQR cost is f(K)=Tr(X(K)Σ)f(K) = \mathrm{Tr}(X(K)\Sigma)f(K)=Tr(X(K)Σ). It equals the expected infinite-horizon quadratic cost when the initial state has covariance Σ\SigmaΣ. Its gradient with respect to the Frobenius inner product ⟨M,N⟩=Tr(M⊤N)\langle M,N\rangle = \mathrm{Tr}(M^\top N)⟨M,N⟩=Tr(M⊤N) is

∇f(K)=2 (RKC−B⊤X(K)) Y(K) C⊤.\nabla f(K) = 2\,(RKC - B^\top X(K))\,Y(K)\,C^\top .∇f(K)=2(RKC−B⊤X(K))Y(K)C⊤.

Given a known stabilizing gain K0∈SK_0\in\mathcal SK0​∈S, the sublevel set is S0={K∈S:f(K)≤f(K0)}\mathcal S_0 = \{K\in\mathcal S : f(K)\le f(K_0)\}S0​={K∈S:f(K)≤f(K0​)}. The gradient flow is the ODE

K˙(t)=−∇f(K(t)),K(0)=K0.\dot K(t) = -\nabla f(K(t)),\qquad K(0) = K_0 .K˙(t)=−∇f(K(t)),K(0)=K0​.

State feedback (SLQR) is the case C=IC = IC=I; there fff is written fSf_SfS​, and K∗K_*K∗​ denotes a minimizer of fSf_SfS​ on S\mathcal SS. Norms: ∥⋅∥F\|\cdot\|_F∥⋅∥F​ is the Frobenius norm and ∥⋅∥\|\cdot\|∥⋅∥ the spectral norm. λ1(M)\lambda_1(M)λ1​(M) is the smallest eigenvalue of a symmetric MMM.

Formalization targets

Goal: Theorem 4.1 for state feedback

For C=IC=IC=I, let L>0L>0L>0 be a Lipschitz constant of ∇f\nabla f∇f on S0\mathcal S_0S0​ and let μ\muμ be the constant (3.11),

μ=λ1(R)λ12(Σ)λ1(Q)8fS(K∗)(∥A∥+∥B∥2fS(K0)/(λ1(Σ)λ1(R)))2.\mu = \frac{\lambda_1(R)\lambda_1^2(\Sigma)\lambda_1(Q)}{8f_S(K_*)\big(\|A\| + \|B\|^2 f_S(K_0)/(\lambda_1(\Sigma)\lambda_1(R))\big)^2}.μ=8fS​(K∗​)(∥A∥+∥B∥2fS​(K0​)/(λ1​(Σ)λ1​(R)))2λ1​(R)λ12​(Σ)λ1​(Q)​.

Then the flow has a solution on [0,∞)[0,\infty)[0,∞), and every solution stays in S0\mathcal S_0S0​, has f(Kt)f(K_t)f(Kt​) nonincreasing, has ∇f(Kt)→0\nabla f(K_t)\to0∇f(Kt​)→0 and min⁡0≤t≤T∥∇f(Kt)∥F2≤f(K0)/T\min_{0\le t\le T}\|\nabla f(K_t)\|_F^2\le f(K_0)/Tmin0≤t≤T​∥∇f(Kt​)∥F2​≤f(K0​)/T, and

∥Kt−K∗∥F≤2L(f(K0)−f(K∗))μ e−μt(t≥0).\|K_t - K_*\|_F \le \frac{\sqrt{2L(f(K_0)-f(K_*))}}{\mu}\,e^{-\mu t}\qquad(t\ge0).∥Kt​−K∗​∥F​≤μ2L(f(K0​)−f(K∗​))​​e−μt(t≥0).

Milestones

In attack order:

  1. Existence of a minimizer (Corollary 3.10).
  2. The gradient formula (Lemma 3.11).
  3. Existence of a Lipschitz constant of ∇f\nabla f∇f on S0\mathcal S_0S0​ (Theorem 3.15, qualitative).
  4. The gradient-domination inequality 12∥∇fS(K)∥F2≥μ(fS(K)−fS(K∗))\tfrac12\|\nabla f_S(K)\|_F^2\ge\mu(f_S(K)-f_S(K_*))21​∥∇fS​(K)∥F2​≥μ(fS​(K)−fS​(K∗​)) on S0\mathcal S_0S0​ (Theorem 3.17).
  5. The energy identity ddtf(Kt)=−∥∇f(Kt)∥F2\tfrac{d}{dt}f(K_t) = -\|\nabla f(K_t)\|_F^2dtd​f(Kt​)=−∥∇f(Kt​)∥F2​.
  6. The integral bound of Appendix D.1.
  7. The output-feedback part of Theorem 4.1 (general CCC with rank⁡C=r\operatorname{rank} C = rrankC=r): existence, invariance of S0\mathcal S_0S0​, monotonicity and (4.2).

Significance

The theorem certifies a simple, model-based procedure: start from any stabilizing gain and follow the negative gradient of the cost. The iterate never loses stability, and it converges exponentially to the optimal gain. The same happens for state feedback even though neither fff nor S\mathcal SS is convex. For output feedback it guarantees convergence to stationarity with an explicit O(1/T)O(1/T)O(1/T) rate. The continuous-time result is the template for the discrete gradient method of the same paper (Theorem 4.2) and for policy-gradient analyses of LQR in learning-based control.

The result is proved in the paper. The paper writes out the proof of (4.2) in Appendix D.1. It describes the whole proof as a replica of Theorems 8 and 9 of Polyak 1963, which treat functions satisfying the Łojasiewicz–Polyak inequality on the whole space. No machine-checked version of any of these statements is known. A formal proof would give the first verified treatment of LQR as an optimization problem over gains. It needs Lyapunov equations, the stabilizing set and the cost, together with the analytic facts on which the policy-gradient literature rests: coercivity, smoothness on sublevel sets, and gradient domination.

Difficulty

The obvious argument is the textbook convergence proof for gradient flows of smooth functions satisfying the Łojasiewicz–Polyak inequality. That proof assumes the function is defined and smooth on the whole space. Here fff lives only on the open set S\mathcal SS, blows up at its boundary, is unbounded on S\mathcal SS and is not globally LLL-smooth. The Łojasiewicz–Polyak inequality holds only on S0\mathcal S_0S0​, with a constant that depends on K0K_0K0​. The work therefore lies in keeping the trajectory inside S0\mathcal S_0S0​ and showing it exists for all time. This requires compactness of S0\mathcal S_0S0​ (coercivity of fff) and a positive distance from S0\mathcal S_0S0​ to the boundary of S\mathcal SS. Local ODE existence alone gives neither. The explicit constant μ\muμ additionally requires lower bounds on solutions of Lyapunov equations and an upper bound on ∥K∥F\|K\|_F∥K∥F​ over S0\mathcal S_0S0​.

Formalization scope

Matrices are Matrix (Fin p) (Fin q) ℝ. Hurwitz means every complex eigenvalue of the complexified matrix has negative real part. X(K)X(K)X(K) and Y(K)Y(K)Y(K) are the unique solutions of their Lyapunov equations. Where the solution is not unique (possible only off S\mathcal SS) they take the value 000, and no statement uses these off-S\mathcal SS values. ∇f\nabla f∇f is defined by formula (3.3), and Lemma 3.11 states that it is the Fréchet derivative with respect to the Frobenius inner product. A solution of the flow is a curve with K(0)=K0K(0)=K_0K(0)=K0​ that stays in S\mathcal SS for t≥0t\ge0t≥0. Its entries have the prescribed derivative within [0,∞)[0,\infty)[0,∞). Global existence and invariance of S0\mathcal S_0S0​ are conclusions, never hypotheses. Assuming a global solution, or a solution confined to S0\mathcal S_0S0​, would trivialize the theorem, and that encoding is excluded. The case C=IC=IC=I is a matrix argument CCC with C=1C=1C=1. λ1\lambda_1λ1​ is the minimum of the (unsorted) eigenvalues, and the spectral norm is λmax⁡(M⊤M)\sqrt{\lambda_{\max}(M^\top M)}λmax​(M⊤M)​. "Monotone decreasing" is rendered as nonincreasing. min⁡0≤t≤T\min_{0\le t\le T}min0≤t≤T​ is rendered as the existence of a point of [0,T][0,T][0,T] where the bound holds.

The standing assumptions of p. 3 are hypotheses wherever they apply: K0∈SK_0\in\mathcal SK0​∈S, Q,R,Σ≻0Q,R,\Sigma\succ0Q,R,Σ≻0, rank⁡C=r\operatorname{rank}C=rrankC=r, and B≠0B\ne0B=0. Deviations from the printed paper:

  • The paper's explicit Lipschitz constant (3.8) is false as printed; the planning notes record counterexamples for both output and state feedback. The goal therefore takes LLL as any Lipschitz constant of ∇f\nabla f∇f on S0\mathcal S_0S0​, which is the paper's own definition of LLL-smoothness (§3.6). Theorem 3.15 enters only in its qualitative form, as the existence of such an LLL.
  • The set-builder for S\mathcal SS on p. 3 writes Rm×n\mathbb R^{m\times n}Rm×n; gains are m×rm\times rm×r.
  • The optimal gain K∗K_*K∗​ is a hypothesis (its existence is Corollary 3.10), and f(K∗)>0f(K_*)>0f(K∗​)>0 is not assumed.

A complete development needs the following: Lyapunov equations and their solution theory (uniqueness, positivity, integral representation), continuity and differentiability of K↦X(K)K\mapsto X(K)K↦X(K) on S\mathcal SS, coercivity of fff, global existence for ODEs confined to a compact invariant set, and the Łojasiewicz–Polyak argument for flows on a subset. The Lyapunov and stabilizing-set layer is reusable across control missions. Proofs of any milestone, and of auxiliary lemmas such as Lemmas 3.8, A.5, C.1–C.3, are welcome.

Selected references

  • I. Fatkhullin, B. Polyak, Optimizing Static Linear Feedback: Gradient Method, SIAM J. Control Optim. 59 (2021); preprint arXiv:2004.09875v2. https://arxiv.org/abs/2004.09875
  • M. Fazel, R. Ge, S. Kakade, M. Mesbahi, Global Convergence of Policy Gradient Methods for the Linear Quadratic Regulator, ICML 2018. https://arxiv.org/abs/1801.05039
  • W. S. Levine, M. Athans, On the determination of the optimal constant output feedback gains for linear multivariable systems, IEEE Trans. Automat. Control 15 (1970). https://doi.org/10.1109/TAC.1970.1099363
  • H. Karimi, J. Nutini, M. Schmidt, Linear Convergence of Gradient and Proximal-Gradient Methods Under the Polyak–Łojasiewicz Condition, ECML PKDD 2016. https://arxiv.org/abs/1608.04636
  • B. T. Polyak, Gradient methods for the minimisation of functionals, USSR Comput. Math. Math. Phys. 3 (1963), 864–878. https://doi.org/10.1016/0041-5553(63)90382-3
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Dynamical SystemsOperations ResearchProbability+1·Captain: mikedeng1

Stabilization of Hybrid Systems by Feedback Control Based on Discrete-Time State Observations I: Almost Sure Asymptotic StabilityResearch Paper

Motivation

Many engineered systems switch between a finite number of operating modes at random times: a power grid after a line failure, a networked controller whose links drop, a manufacturing plant whose machines break down and are repaired. A standard model for such systems is a hybrid stochastic differential equation, also called an SDE with Markovian switching: the state follows an Itô equation whose coefficients depend on a mode that evolves as a continuous-time Markov chain. The monograph of Mao and Yuan (Stochastic Differential Equations with Markovian Switching, 2006) develops the stability theory of these equations.

A controller that stabilizes such a system usually needs the current state. In practice the state is sampled: it is observed at times 0,τ,2τ,…0,\tau,2\tau,\dots0,τ,2τ,… and the control is held between observations. Mao (Automatica 49, 2013) showed that, under a global Lipschitz condition on the drift and diffusion, a feedback control based on discrete-time observations stabilizes a hybrid SDE in the sense of mean-square exponential stability when τ\tauτ is small enough. You, Liu, Lu, Mao and Qiu (SIAM J. Control Optim. 53(2), 2015) replaced that condition by local Lipschitz continuity plus linear growth, gave an explicit bound (3.5) on the admissible observation interval τ\tauτ, and proved H∞H_\inftyH∞​-stability, mean-square asymptotic stability, almost sure asymptotic stability and exponential stability of the controlled system. This mission formalizes the almost sure asymptotic stability result, Theorem 3.4, and the results it is built on.

Setting

Let (Ω,F,{Ft}t≥0,P)(\Omega,\mathcal F,\{\mathcal F_t\}_{t\ge0},\mathbb P)(Ω,F,{Ft​}t≥0​,P) be a probability space with a filtration satisfying the usual conditions (increasing, right-continuous, F0\mathcal F_0F0​ contains the null sets). On it live an mmm-dimensional {Ft}\{\mathcal F_t\}{Ft​}-Brownian motion www and a right-continuous {Ft}\{\mathcal F_t\}{Ft​}-Markov chain rrr on S={1,…,N}S=\{1,\dots,N\}S={1,…,N} with generator Γ=(γij)\Gamma=(\gamma_{ij})Γ=(γij​) (γij≥0\gamma_{ij}\ge0γij​≥0 for i≠ji\ne ji=j, zero row sums), independent of www. Fix τ>0\tau>0τ>0 and the sampling time δt=[t/τ]τ\delta_t=[t/\tau]\tauδt​=[t/τ]τ, the last observation time up to ttt. The controlled system is

dx(t)=(f(x(t),r(t),t)+u(x(δt),r(t),t))dt+g(x(t),r(t),t) dw(t),x(0)=x0, r(0)=r0,(2.1)dx(t)=\big(f(x(t),r(t),t)+u(x(\delta_t),r(t),t)\big)dt+g(x(t),r(t),t)\,dw(t),\qquad x(0)=x_0,\ r(0)=r_0,\tag{2.1}dx(t)=(f(x(t),r(t),t)+u(x(δt​),r(t),t))dt+g(x(t),r(t),t)dw(t),x(0)=x0​, r(0)=r0​,(2.1)

with f,u:Rn×S×R+→Rnf,u:\mathbb R^n\times S\times\mathbb R_+\to\mathbb R^nf,u:Rn×S×R+​→Rn and g:Rn×S×R+→Rn×mg:\mathbb R^n\times S\times\mathbb R_+\to\mathbb R^{n\times m}g:Rn×S×R+​→Rn×m. The feedback uuu sees the state only at the observation times.

The hypotheses are:

  • Assumption 2.1: f,gf,gf,g locally Lipschitz in xxx, and ∣f(x,i,t)∣≤K1∣x∣|f(x,i,t)|\le K_1|x|∣f(x,i,t)∣≤K1​∣x∣, ∣g(x,i,t)∣≤K2∣x∣|g(x,i,t)|\le K_2|x|∣g(x,i,t)∣≤K2​∣x∣ (∣g∣|g|∣g∣ the trace norm).
  • Assumption 2.2: ∣u(x,i,t)−u(y,i,t)∣≤K3∣x−y∣|u(x,i,t)-u(y,i,t)|\le K_3|x-y|∣u(x,i,t)−u(y,i,t)∣≤K3​∣x−y∣ and u(0,i,t)=0u(0,i,t)=0u(0,i,t)=0.
  • Assumption 3.1: there are U∈C2,1(Rn×S×R+;R+)U\in C^{2,1}(\mathbb R^n\times S\times\mathbb R_+;\mathbb R_+)U∈C2,1(Rn×S×R+​;R+​) and λ1,λ2>0\lambda_1,\lambda_2>0λ1​,λ2​>0 with LU(x,i,t)+λ1∣Ux(x,i,t)∣2≤−λ2∣x∣2\mathcal LU(x,i,t)+\lambda_1|U_x(x,i,t)|^2\le-\lambda_2|x|^2LU(x,i,t)+λ1​∣Ux​(x,i,t)∣2≤−λ2​∣x∣2, where
LU=Ut+Ux[f+u]+12trace⁡[gTUxxg]+∑jγijU(x,j,t).\mathcal LU=U_t+U_x[f+u]+\tfrac12\operatorname{trace}[g^TU_{xx}g]+\sum_j\gamma_{ij}U(x,j,t).LU=Ut​+Ux​[f+u]+21​trace[gTUxx​g]+j∑​γij​U(x,j,t).
  • Condition (3.5): λ2>τK32λ1[2τ(K12+2K32)+K22]\lambda_2>\frac{\tau K_3^2}{\lambda_1}\big[2\tau(K_1^2+2K_3^2)+K_2^2\big]λ2​>λ1​τK32​​[2τ(K12​+2K32​)+K22​] and τ≤14K3\tau\le\frac1{4K_3}τ≤4K3​1​.

In Lean these are Assumption21, Assumption22, C21, LU, Assumption31, Condition35, in the namespace You2015.Asymp; the basis is HybridSetup, the Itô integral IsItoIntegral, the sampling time delta, and solutions SolvesSampledHybridSDE, in the namespace You2015.Shared shared with the companion mission.

Formalization targets

Goal: Theorem 3.4 (almost sure asymptotic stability)

Under the hypotheses above, every solution of (2.1) satisfies

lim⁡t→∞x(t)=0a.s.\lim_{t\to\infty}x(t)=0\quad\text{a.s.}t→∞lim​x(t)=0a.s.

for all x0∈Rnx_0\in\mathbb R^nx0​∈Rn and r0∈Sr_0\in Sr0​∈S. No rate is claimed; the statement is the qualitative convergence of almost every path.

Milestones, in the order the proof uses them

  1. (3.15) E∣x(t)−x(δt)∣2≤2E∫δtt[τ∣f+u(x(δs),⋅)∣2+∣g∣2]ds\mathbb E|x(t)-x(\delta_t)|^2\le2\mathbb E\int_{\delta_t}^t[\tau|f+u(x(\delta_s),\cdot)|^2+|g|^2]dsE∣x(t)−x(δt​)∣2≤2E∫δt​t​[τ∣f+u(x(δs​),⋅)∣2+∣g∣2]ds.
  2. Theorem 3.2 (H∞H_\inftyH∞​-stability): ∫0∞E∣x(s)∣2ds<∞\int_0^\infty\mathbb E|x(s)|^2ds<\infty∫0∞​E∣x(s)∣2ds<∞.
  3. (3.21) E∣x(s)−x(δs)∣2≤3(τK12+K22)1−6τ2K32∫δssE∣x(z)∣2dz+6τ2K321−6τ2K32E∣x(s)∣2\mathbb E|x(s)-x(\delta_s)|^2\le\frac{3(\tau K_1^2+K_2^2)}{1-6\tau^2K_3^2}\int_{\delta_s}^s\mathbb E|x(z)|^2dz+\frac{6\tau^2K_3^2}{1-6\tau^2K_3^2}\mathbb E|x(s)|^2E∣x(s)−x(δs​)∣2≤1−6τ2K32​3(τK12​+K22​)​∫δs​s​E∣x(z)∣2dz+1−6τ2K32​6τ2K32​​E∣x(s)∣2.
  4. (3.23) sup⁡t≥0E∣x(t)∣2<∞\sup_{t\ge0}\mathbb E|x(t)|^2<\inftysupt≥0​E∣x(t)∣2<∞.
  5. ∣E∣x(t2)∣2−E∣x(t1)∣2∣≤C(t2−t1)|\mathbb E|x(t_2)|^2-\mathbb E|x(t_1)|^2|\le C(t_2-t_1)∣E∣x(t2​)∣2−E∣x(t1​)∣2∣≤C(t2​−t1​).
  6. Theorem 3.3: lim⁡t→∞E∣x(t)∣2=0\lim_{t\to\infty}\mathbb E|x(t)|^2=0limt→∞​E∣x(t)∣2=0.
  7. (3.24)–(3.25): E∫0∞∣x(t)∣2dt<∞\mathbb E\int_0^\infty|x(t)|^2dt<\inftyE∫0∞​∣x(t)∣2dt<∞ and lim inf⁡t→∞∣x(t)∣=0\liminf_{t\to\infty}|x(t)|=0liminft→∞​∣x(t)∣=0 a.s.
  8. (3.28): P(∃t:∣x(t)∣≥h)≤C/h2\mathbb P(\exists t:|x(t)|\ge h)\le C/h^2P(∃t:∣x(t)∣≥h)≤C/h2 for h>∣x0∣h>|x_0|h>∣x0​∣.

Significance

The result. Theorem 3.4 says that a controller sampling the state at rate 1/τ1/\tau1/τ makes almost every trajectory of the switching system converge to the equilibrium, with an explicit, checkable bound (3.5) on τ\tauτ. Mean-square convergence (Theorem 3.3) does not imply almost sure convergence in general, and a single trajectory is what an operator observes, so the pathwise statement is the one relevant to a deployed system. Condition (3.5) is stated in terms of the constants of Assumptions 2.1, 2.2 and 3.1, so for a concrete system (Section 6 of the paper) it gives a numerical bound on the observation interval.

Formalizing it. The results are proved in the paper; none of them is machine-checked. Mathlib has real Brownian motion but no Itô integral, no stochastic differential equations and no continuous-time Markov chains. The mission therefore also produces a reusable definition layer: a filtration under the usual conditions, a multidimensional {Ft}\{\mathcal F_t\}{Ft​}-Brownian motion, an {Ft}\{\mathcal F_t\}{Ft​}-Markov chain with a given generator, the L2L^2L2 Itô integral of vector-valued integrands, and the solution notion of an SDE with Markovian switching and a sampled-state delay. A related but different layer exists on Prove2Me for Ethier–Kurtz (EthierKurtz_IsStandardBrownian, EthierKurtz_HasBrownianItoIntegral, EthierKurtz_SolvesBrownianSDE); it has no mode switching and no sampled state, so it cannot express (2.1).

Difficulty

Equation (2.1) is a stochastic differential delay equation with the delay t−δtt-\delta_tt−δt​, which is bounded but jumps at every observation time and has derivative 111 in between. The stability theorems for hybrid delay equations in the literature require a differentiable delay with derivative less than one (Mao–Yuan, p. 285), so they do not apply. Applying LU\mathcal LULU directly to U(x(t),r(t),t)U(x(t),r(t),t)U(x(t),r(t),t) leaves the term Ux[u(x(t))−u(x(δt))]U_x[u(x(t))-u(x(\delta_t))]Ux​[u(x(t))−u(x(δt​))], which has no sign and depends on the path over a whole observation interval, so a Lyapunov function of the current state alone does not close the argument.

For the goal, the natural first idea, deducing almost sure convergence from E∣x(t)∣2→0\mathbb E|x(t)|^2\to0E∣x(t)∣2→0 or from ∫0∞∣x(t)∣2dt<∞\int_0^\infty|x(t)|^2dt<\infty∫0∞​∣x(t)∣2dt<∞ a.s., fails: both are compatible with paths that make ever shorter excursions away from 000. The obstacle is to exclude infinitely many excursions of a fixed size, which neither moment statement controls.

Formalization scope

Conventions committed to in Lean:

  • The state space is EuclideanSpace ℝ (Fin n), so ∣x∣|x|∣x∣ is the Euclidean norm; the explicit constants in (3.5) and (3.21) depend on it. The diffusion ggg is given by its mmm columns and ∣g∣2=∑k∣gk∣2|g|^2=\sum_k|g_k|^2∣g∣2=∑k​∣gk​∣2 (trace norm). Modes are Fin N (0-based). Time is ℝ≥0; time integrals are over subsets of R\mathbb RR at s.toNNReal.
  • Every expectation E∣⋅∣2\mathbb E|\cdot|^2E∣⋅∣2 and every time integral of a nonnegative quantity is a lower Lebesgue integral in [0,∞][0,\infty][0,∞], so a non-integrable process cannot produce a junk value 000.
  • "The solution of (2.1)" is read as every process satisfying the solution definition: progressively measurable, almost surely continuous paths, E∣x(t)∣2<∞\mathbb E|x(t)|^2<\inftyE∣x(t)∣2<∞ for each ttt, and for each ttt, almost surely, the integral equation with Itô integrals in the L2L^2L2 sense. Existence and uniqueness (cited from Mao–Yuan on p. 908) are not asserted.
  • "An mmm-dimensional Brownian motion" and "a Markov chain with generator Γ\GammaΓ" are read in the Mao–Yuan framework the paper cites: an {Ft}\{\mathcal F_t\}{Ft​}-Brownian motion with independent coordinates and increments independent of the past, and an {Ft}\{\mathcal F_t\}{Ft​}-Markov chain with transition matrix etΓe^{t\Gamma}etΓ. The usual conditions are kept as hypotheses.
  • "Locally Lipschitz" is uniform in the mode and time on each ball. C2,1C^{2,1}C2,1 carries its derivatives Ut,Ux,UxxU_t,U_x,U_{xx}Ut​,Ux​,Uxx​ as witnesses tied to UUU by derivative relations and joint continuity.
  • "τ>0\tau>0τ>0 sufficiently small for (3.5)" means every τ>0\tau>0τ>0 satisfying both inequalities of (3.5). U,λ1,λ2,τU,\lambda_1,\lambda_2,\tauU,λ1​,λ2​,τ are data of each statement. The paper's "CCC denotes a positive constant" is an existential chosen after x0x_0x0​, r0r_0r0​ and the solution, and before the time variables and hhh.
  • (3.15) and (3.21) are stated under fewer hypotheses than the surrounding proof has (Assumptions 2.1, 2.2, τ>0\tau>0τ>0, and for (3.21) τ≤1/(4K3)\tau\le1/(4K_3)τ≤1/(4K3​)), because their derivations use no more. Misprints on the page (for example g(x,i,s)=f(x,i,0)g(x,i,s)=f(x,i,0)g(x,i,s)=f(x,i,0) on p. 909 and the swapped definitions of ∨,∧\vee,\wedge∨,∧ on p. 907) are not formalized.

A trivializing formalization is ruled out: the expectations are not Bochner integrals (which vanish for non-integrable integrands), the solution notion admits the true solution and requires path continuity, the derivative witnesses of UUU are tied to UUU, and a sorry-free check shows that the data hypotheses (Assumptions 2.1, 2.2, 3.1, C2,1C^{2,1}C2,1, (3.5)) are satisfiable, for example by n=m=N=1n=m=N=1n=m=N=1, f=g=0f=g=0f=g=0, u(x)=−xu(x)=-xu(x)=−x, U=∣x∣2U=|x|^2U=∣x∣2, λ1=1/4\lambda_1=1/4λ1​=1/4, λ2=1\lambda_2=1λ2​=1, τ=1/10\tau=1/10τ=1/10.

Welcome contributions: the Itô isometry and Itô's formula for the L2L^2L2 integral defined here, a generalized Itô formula for functions of a Markov-modulated Itô process, and Doob's maximal inequality in continuous time. These are reusable far beyond this mission. Section 4 of the paper (exponential stability) is a separate mission of the same series.

Selected references

  • S. You, W. Liu, J. Lu, X. Mao, Q. Qiu, Stabilization of Hybrid Systems by Feedback Control Based on Discrete-Time State Observations, SIAM J. Control Optim. 53(2), 905–925, 2015. https://doi.org/10.1137/140985779
  • X. Mao, C. Yuan, Stochastic Differential Equations with Markovian Switching, Imperial College Press, 2006. https://doi.org/10.1142/p473
  • X. Mao, Stabilization of continuous-time hybrid stochastic differential equations by discrete-time feedback control, Automatica 49(12), 3677–3681, 2013. https://doi.org/10.1016/j.automatica.2013.09.005
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Operations ResearchOptimizationProbability+1·Captain: mikedeng1

A General Stochastic Maximum Principle for Optimal Control Problems: The Maximum Principle with First- and Second-Order Adjoint ProcessesResearch Paper

Motivation

Pontryagin's maximum principle gives necessary conditions for optimality in deterministic optimal control: along an optimal trajectory, the optimal control maximizes (or minimizes) a Hamiltonian built from an adjoint process. For a system driven by Brownian noise the analogous statement was open in full generality for two decades. The difficulty appears exactly when the diffusion coefficient depends on the control and the control domain is not convex, the situation of controlled volatility in finance, of controlled noise intensity in engineering, and of any problem whose admissible actions form a discrete or otherwise nonconvex set.

Shige Peng's 1990 paper (SIAM J. Control Optim. 28(4)) closed that case. It introduced the second-order adjoint process and a second-order variational inequality, and it is the starting point of the modern theory of stochastic Hamiltonian systems and of backward stochastic differential equations as a tool in control.

Timeline.

  • 1972: Kushner obtains necessary conditions for diffusions whose diffusion coefficient does not depend on the control (SIAM J. Control 10).
  • 1973–1978: Bismut introduces the adjoint equation as a linear backward stochastic differential equation and develops duality methods (SIAM Review 20).
  • Early 1980s: Bensoussan and Haussmann prove maximum principles for convex control domains or control-independent diffusion, using the first-order adjoint equation only.
  • 1990: Peng proves the general principle, with control-dependent diffusion and an arbitrary nonempty control domain (this mission). In the same year Pardoux and Peng prove existence and uniqueness for nonlinear backward SDEs (Systems Control Lett. 14).
  • 1999: Yong and Zhou give a textbook account of the theory (Springer).

Setting

Let (Ω,F,P)(\Omega,\mathcal F,P)(Ω,F,P) be a probability space carrying a standard ddd-dimensional Wiener process B=(B1,…,Bd)B=(B^1,\dots,B^d)B=(B1,…,Bd), and let Ft=σ{B(s);0≤s≤t}\mathcal F^t=\sigma\{B(s);0\le s\le t\}Ft=σ{B(s);0≤s≤t} be its natural filtration. Fix a horizon T>0T>0T>0, an initial state x0∈Rnx_0\in\mathbb R^nx0​∈Rn and a nonempty control domain U⊆RkU\subseteq\mathbb R^kU⊆Rk. The data are

g:Rn×Rk→Rn,σ=(σ1,…,σd), σj:Rn×Rk→Rn,l:Rn×Rk→R,h:Rn→R.g:\mathbb R^n\times\mathbb R^k\to\mathbb R^n,\quad \sigma=(\sigma^1,\dots,\sigma^d),\ \sigma^j:\mathbb R^n\times\mathbb R^k\to\mathbb R^n,\quad l:\mathbb R^n\times\mathbb R^k\to\mathbb R,\quad h:\mathbb R^n\to\mathbb R .g:Rn×Rk→Rn,σ=(σ1,…,σd), σj:Rn×Rk→Rn,l:Rn×Rk→R,h:Rn→R.

An admissible control vvv is a progressively measurable UUU-valued process with sup⁡t≤TE∣v(t)∣m<∞\sup_{t\le T}E|v(t)|^m<\inftysupt≤T​E∣v(t)∣m<∞ for every m≥1m\ge1m≥1. Its trajectory solves the state equation

dx(t)=g(x(t),v(t)) dt+∑j=1dσj(x(t),v(t)) dBj(t),x(0)=x0,dx(t)=g(x(t),v(t))\,dt+\sum_{j=1}^d\sigma^j(x(t),v(t))\,dB^j(t),\qquad x(0)=x_0,dx(t)=g(x(t),v(t))dt+j=1∑d​σj(x(t),v(t))dBj(t),x(0)=x0​,

and its cost is J(v)=E∫0Tl(x(t),v(t)) dt+E h(x(T))J(v)=E\int_0^Tl(x(t),v(t))\,dt+E\,h(x(T))J(v)=E∫0T​l(x(t),v(t))dt+Eh(x(T)). A pair (y,u)(y,u)(y,u) is optimal when J(u)≤J(v)J(u)\le J(v)J(u)≤J(v) for every admissible vvv.

Assumption (3): g,σ,l,hg,\sigma,l,hg,σ,l,h are C2C^2C2 in xxx, jointly continuous in (x,v)(x,v)(x,v) together with their first and second xxx-derivatives; gx,gxx,σx,σxx,lxx,hxxg_x,g_{xx},\sigma_x,\sigma_{xx},l_{xx},h_{xx}gx​,gxx​,σx​,σxx​,lxx​,hxx​ are bounded; and g,σ,lx,hxg,\sigma,l_x,h_xg,σ,lx​,hx​ grow at most like C(1+∣x∣+∣v∣)C(1+|x|+|v|)C(1+∣x∣+∣v∣).

The Hamiltonian is H(x,v,p,K)=l(x,v)+(p,g(x,v))+∑j(Kj,σj(x,v))H(x,v,p,K)=l(x,v)+(p,g(x,v))+\sum_j(K_j,\sigma^j(x,v))H(x,v,p,K)=l(x,v)+(p,g(x,v))+∑j​(Kj​,σj(x,v)). The first-order adjoint process (p,K)(p,K)(p,K) solves the backward equation

−dp=[gx∗p+∑jσxj∗Kj+lx]dt−∑jKj dBj,p(T)=hx(y(T)),-dp=\Big[g_x^*p+\sum_j\sigma_x^{j*}K_j+l_x\Big]dt-\sum_jK_j\,dB^j,\qquad p(T)=h_x(y(T)),−dp=[gx∗​p+j∑​σxj∗​Kj​+lx​]dt−j∑​Kj​dBj,p(T)=hx​(y(T)),

and the second-order adjoint process (P,Q)(P,Q)(P,Q), symmetric-matrix valued, solves

−dP=[gx∗P+Pgx+∑jσxj∗Pσxj+∑jσxj∗Qj+∑jQjσxj+Hxx]dt−∑jQj dBj,P(T)=hxx(y(T)),-dP=\Big[g_x^*P+Pg_x+\sum_j\sigma_x^{j*}P\sigma_x^j+\sum_j\sigma_x^{j*}Q_j+\sum_jQ_j\sigma_x^j+H_{xx}\Big]dt-\sum_jQ_j\,dB^j,\qquad P(T)=h_{xx}(y(T)),−dP=[gx∗​P+Pgx​+j∑​σxj∗​Pσxj​+j∑​σxj∗​Qj​+j∑​Qj​σxj​+Hxx​]dt−j∑​Qj​dBj,P(T)=hxx​(y(T)),

with all coefficients evaluated along (y(t),u(t))(y(t),u(t))(y(t),u(t)) and both solutions adapted to Ft\mathcal F^tFt.

Formalization targets

Goal: Theorem 3 (p. 975)

If (y,u)(y,u)(y,u) is optimal, then adjoint processes (p,K)(p,K)(p,K) and (P,Q)(P,Q)(P,Q) exist in LF2L^2_{\mathcal F}LF2​, solving the two equations above, such that for every v∈Uv\in Uv∈U, for almost every τ∈[0,T]\tau\in[0,T]τ∈[0,T], almost surely,

H(y,v,p,K−Pσ(y,u))+12tr⁡(σσ∗(y,v)P) ≥ H(y,u,p,K−Pσ(y,u))+12tr⁡(σσ∗(y,u)P),H\big(y,v,p,K-P\sigma(y,u)\big)+\tfrac12\operatorname{tr}\big(\sigma\sigma^*(y,v)P\big)\ \ge\ H\big(y,u,p,K-P\sigma(y,u)\big)+\tfrac12\operatorname{tr}\big(\sigma\sigma^*(y,u)P\big),H(y,v,p,K−Pσ(y,u))+21​tr(σσ∗(y,v)P) ≥ H(y,u,p,K−Pσ(y,u))+21​tr(σσ∗(y,u)P),

all evaluated at time τ\tauτ.

Milestones

  1. Lemma 1: the spike-perturbed state equals y+y1+y2y+y_1+y_2y+y1​+y2​ up to o(ε2)o(\varepsilon^2)o(ε2) in mean square, where y1,y2y_1,y_2y1​,y2​ solve the first- and second-order variational equations (5), (6).
  2. Lemma 2: the cost expansion (11) is ≥o(ε)\ge o(\varepsilon)≥o(ε) at an optimal control.
  3. Eq. (13): existence and uniqueness of (p,K)(p,K)(p,K) as a Riesz representer.
  4. Eq. (14): the cost expansion in Hamiltonian form is ≥o(ε)\ge o(\varepsilon)≥o(ε).
  5. Eq. (17): existence and uniqueness of (P,Q)(P,Q)(P,Q) as a Riesz representer.
  6. Eq. (18): the variational inequality for these representers.
  7. Eq. (19): (p,K)(p,K)(p,K) is the unique solution of the first-order adjoint equation.
  8. Eq. (20): (P,Q)(P,Q)(P,Q) solves the second-order adjoint equation.

Significance

The result. Theorem 3 is the necessary condition for optimal control of diffusions in its general form. When σ\sigmaσ does not depend on the control the trace terms cancel and it reduces to the classical first-order principle. When the control enters the diffusion, the first-order condition is false in general, and the second-order adjoint PPP is the correction. The theorem underlies stochastic linear-quadratic theory, the verification of optimal portfolio and volatility-control policies, and the relation between the maximum principle and the Hamilton–Jacobi–Bellman equation.

Formalizing it. The theorem is classical and proved; none of it is machine-checked. Mathlib has real Brownian motion but no stochastic integral, no SDE and no backward SDE. This mission produces the first formal statements on the platform of a controlled SDE, of a backward SDE and of the maximum principle, together with a precise definition layer (Itô integral, Itô process, BSDE solution) that later missions can reuse, e.g. for Peng's endpoint-constrained principle (§6 of the paper) or for the existence theory of BSDEs. A formal proof would also pin down the approximation arguments the paper leaves to the reader.

Difficulty

The obvious route perturbs the optimal control convexly, u+ε(v−u)u+\varepsilon(v-u)u+ε(v−u), and differentiates the cost. That needs UUU convex. For nonconvex UUU one uses a spike variation on a time interval of length ε\varepsilonε. For deterministic systems the state then moves by O(ε)O(\varepsilon)O(ε) and a first-order expansion suffices. With control-dependent diffusion the stochastic integral over the spike interval moves the state by order ε\sqrt\varepsilonε​ in L2L^2L2, so the first-order variational equation leaves an error of the same order as the effect being measured. Second-order terms in the state enter the cost at order ε\varepsilonε, and they are quadratic, so they cannot be handled by a single linear adjoint. The second-order expansion, the matrix-valued adjoint that represents the quadratic term, and the identification of both adjoints with backward SDEs are where the work lies. On the formal side, none of the stochastic calculus exists in Mathlib: the Itô isometry, Itô's formula for matrix-valued processes, moment estimates for linear SDEs and the martingale representation behind the backward equations all have to be built.

Formalization scope

Conventions committed to in Lean:

  • States, controls and noise are Fin n → ℝ, Fin k → ℝ, Fin d → ℝ with the sup norm; matrices are Matrix (Fin n) (Fin n) ℝ. Time is ℝ≥0, and time integrals are over [0, t] ⊂ ℝ.
  • The Wiener process is Rd\mathbb R^dRd-valued: the paper's "RnR^nRn-valued standard Wiener process" (p. 967) is a misprint, since σ(x,v)∈L(Rd,Rn)\sigma(x,v)\in\mathcal L(R^d,R^n)σ(x,v)∈L(Rd,Rn). Coordinates are independent real Brownian motions (Mathlib's IsBrownianReal).
  • The filtration is the natural filtration of BBB, not completed, as on p. 967.
  • "Adapted", for processes integrated in dtdtdt, is read as progressively measurable.
  • The Itô integral is a relation (an L2L^2L2 limit of elementary integrals, as in Ikeda–Watanabe), not an operator. SDE and BSDE solutions hold "for every ttt, almost surely", with sup⁡tE∣x(t)∣2<∞\sup_tE|x(t)|^2<\inftysupt​E∣x(t)∣2<∞ for forward solutions and LF2L^2_{\mathcal F}LF2​ membership for backward ones.
  • Optimality is among admissible controls of finite cost, and the optimal cost is finite; the paper never states finiteness, and a cost can be +∞+\infty+∞ under (3).
  • Lemma 1 is stated with o(ε2)o(\varepsilon^2)o(ε2) where the page prints "≤Cε2\le C\varepsilon^2≤Cε2" in (4). The proof (via (10)) establishes o(ε2)o(\varepsilon^2)o(ε2), and Lemma 2 needs it. Lemma 1, (13), (17), (19) and (20) are stated for any admissible pair, since their proofs do not use optimality.
  • "≥o(ε)\ge o(\varepsilon)≥o(ε)" means: some r(ε)=o(ε)r(\varepsilon)=o(\varepsilon)r(ε)=o(ε) as ε→0+\varepsilon\to0^+ε→0+ bounds the left side from below for small ε\varepsilonε. "∀v∈U\forall v\in U∀v∈U, a.e., a.s." quantifies vvv first, then τ\tauτ, then ω\omegaω.
  • PPP and QjQ_jQj​ are symmetric-valued (Rn,nR^{n,n}Rn,n is the space of symmetric matrices, p. 973). Stochastic integrals against the matrix σ\sigmaσ or QQQ are sums over the columns, ∑j(⋅)j dBj\sum_j(\cdot)_j\,dB^j∑j​(⋅)j​dBj.

Trivializing formalizations ruled out. Without adaptedness the backward equations have pathwise solutions with K=0K=0K=0 and the goal would be free; every adjoint and every solution is required to be progressive for the natural filtration of BBB. The hypotheses are satisfiable: a sorry-free check shows that the zero problem has an optimal pair and that the Itô relation holds for the zero integrand.

Infrastructure needed, and reusable. The Itô integral and isometry, Itô's formula (vector and matrix forms), existence, uniqueness and moment estimates for linear SDEs with bounded coefficients, Riesz representation in LF2L^2_{\mathcal F}LF2​, and existence and uniqueness for linear BSDEs (via martingale representation for the Brownian filtration). All of these are reusable well beyond this mission; contributions of any of them, as separate theorems, are welcome. Related platform definitions: the Ethier–Kurtz series (EthierKurtz_HasBrownianItoIntegral, EthierKurtz_SolvesBrownianSDE) formalizes an Itô integral by dyadic step approximation and uncontrolled SDEs over a completed filtration. The deterministic Pontryagin principle appears in Vector Space Methods XII and Dynamic Programming and Optimal Control III.

Selected references

  • S. Peng, A General Stochastic Maximum Principle for Optimal Control Problems, SIAM J. Control Optim. 28(4), 966–979, 1990. https://doi.org/10.1137/0328054
  • H. J. Kushner, Necessary Conditions for Continuous Parameter Stochastic Optimization Problems, SIAM J. Control 10(3), 550–565, 1972. https://doi.org/10.1137/0310041
  • J.-M. Bismut, An Introductory Approach to Duality in Optimal Stochastic Control, SIAM Review 20(1), 62–78, 1978. https://doi.org/10.1137/1020004
  • E. Pardoux and S. Peng, Adapted Solution of a Backward Stochastic Differential Equation, Systems & Control Letters 14(1), 55–61, 1990. https://doi.org/10.1016/0167-6911(90)90082-6
  • J. Yong and X. Y. Zhou, Stochastic Controls: Hamiltonian Systems and HJB Equations, Springer, 1999. https://doi.org/10.1007/978-1-4612-1466-3
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