Title :
Control system design for Hypersonic Reentry Vehicle driven by RCS based on modified Phase Plane Method
Author :
Liang Dong ; Song Jian-mei ; Cai Gao-hua
Author_Institution :
Key Lab. of Dynamics & Control of Flight Vehicle, Beijing Inst. of Technol., Beijing, China
Abstract :
An angle-of-attack control system for Hypersonic Reentry Vehicle driven by Reaction Control System (RCS) is designed based on Phase Plane Method (MPPM) in this paper. Firstly, the model of Hypersonic Reentry Vehicle and the RCS model are introduced. Then the design method for the modified phase plane controller is presented in detail. Finally, the performance of the designed controller is demonstrated by simulation with linear model of Hypersonic Reentry Vehicle, which shows that the effectiveness and rationality of the modified phase plane controller.
Keywords :
aircraft control; control system synthesis; missile control; MPPM; RCS model; angle-of-attack control system; control system design; hypersonic reentry vehicle; linear model; modified phase plane controller method; reaction control system; Aerodynamics; Computer aided instruction; Control systems; Electronic mail; Laboratories; Vehicle dynamics; Vehicles; Hypersonic Reentry Vehicle (HRV); Modified Phase Plane Method (MPPM); Reaction Control System (RCS);
Conference_Titel :
Control Conference (CCC), 2013 32nd Chinese
Conference_Location :
Xi´an
