Time-varying sliding mode control of missile based on suboptimal method

doi:10.23919/JSEE.2021.000060

Abstract

Abstract:

This paper proposes a time-varying sliding mode control method to address nonlinear missile body kinematics based on the suboptimal control theory. The analytical solution of suboptimal time-varying sliding surface and the corresponding suboptimal control law are obtained by solving the state-dependent Riccati equation analytically. Then, the Lyapunov method is used to analyze the motion trend in sliding surface and the asymptotic stability of the closed-loop system is validated. The suboptimal control law is transformed to the form of pseudo-angle-of-attack feedback. The simulation results indicate that the satisfactory performance can be obtained and the control law can overcome the influence of parameter errors.

Key words: suboptimal control, Riccati equation, analytic solution, sliding mode control, nonlinear control

Zongxing LI, Rui ZHANG. Time-varying sliding mode control of missile based on suboptimal method[J]. Journal of Systems Engineering and Electronics, 2021, 32(3): 700-710.

Figures/Tables 10

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