期刊
IEEE TRANSACTIONS ON AUTOMATIC CONTROL
卷 66, 期 10, 页码 4731-4746出版社
IEEE-INST ELECTRICAL ELECTRONICS ENGINEERS INC
DOI: 10.1109/TAC.2020.3038402
关键词
LMIs; nonlinear systems; optimization algorithms; robust control; stochastic optimal control
资金
- Jet Propulsion Laboratory, California Institute of Technology
- Raytheon Company
CV-STEM is a state feedback control framework that computes the control input by greedily minimizing an upper bound of the steady-state mean squared tracking error of the system trajectories, providing a sufficient guarantee for exponential boundedness of the error with L-2-robustness properties. Validation shows its superiority over PID, H-infinity, and baseline nonlinear controllers in spacecraft attitude control and synchronization problems.
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.
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