2002•Journal of Projectiles.Rockets.Missiles and GuidanceRequires access

Backstepping Control Based Autopilot Design for Reentry Aerocraft

Lian Bao

Abstract

In this paper, a new kind of control strategy for design of autopilot with nonlinear feedback based on backstepping technique was presented. Also the autopilot of reentry aerocraft was designed with this nethod. The simulation results show that the method of backstepping proposed in this paper is efficient. The design process is simplex than others and easy for implement.

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Available abstract

Key concepts: Autopilot, Backstepping, Reentry, Control theory (sociology), Computer science, Control engineering, Nonlinear system, Process (computing)