DocumentCode
1709641
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
fYear
2013
Firstpage
2372
Lastpage
2376
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);
fLanguage
English
Publisher
ieee
Conference_Titel
Control Conference (CCC), 2013 32nd Chinese
Conference_Location
Xi´an
Type
conf
Filename
6639823
Link To Document