Robust Controller Design for Stochastic Nonlinear Systems via Convex Optimization

被引:32
|
作者
Tsukamoto, Hiroyasu [1 ]
Chung, Soon-Jo [2 ]
机构
[1] CALTECH, Aerosp, Pasadena, CA 91125 USA
[2] CALTECH, Dept Aerosp GALCIT, Pasadena, CA 91125 USA
关键词
LMIs; nonlinear systems; optimization algorithms; robust control; stochastic optimal control; H-INFINITY-CONTROL; DEPENDENT RICCATI EQUATION; MODEL-PREDICTIVE CONTROL; OPTIMAL FEEDBACK-CONTROL; H-2/H-INFINITY CONTROL; CONTRACTION ANALYSIS; SYNCHRONIZATION; STABILIZATION; SPACECRAFT; STABILITY;
D O I
10.1109/TAC.2020.3038402
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
This article presents ConVex optimization-based Stochastic steady-state Tracking Error Minimization (CV-STEM), a new state feedback control framework for a class of Ito stochastic nonlinear systems and Lagrangian systems. Its innovation lies in computing the control input by an optimal contraction metric, which greedily minimizes an upper bound of the steady-state mean squared tracking error of the system trajectories. Although the problem of minimizing the bound is nonconvex, its equivalent convex formulation is proposed utilizing SDC parameterizations of the nonlinear system equation. It is shown using stochastic incremental contraction analysis that the CV-STEM provides a sufficient guarantee for exponential boundedness of the error for all time with L-2-robustness properties. For the sake of its sampling-based implementation, we present discrete-time stochastic contraction analysis with respect to a state- and time-dependent metric along with its explicit connection to continuous-time cases. We validate the superiority of the CV-STEM to PID, H-infinity, and baseline nonlinear controllers for spacecraft attitude control and synchronization problems.
引用
收藏
页码:4731 / 4746
页数:16
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