DocumentCode
2241544
Title
A decomposition approach to design attitude controller for underactuated reentry vehicle
Author
Wenming, Nie ; Zhi, Wang ; Huifeng, Li
Author_Institution
School of Astronautics, BeiHang University, Beijing 100191, P.R. China
fYear
2015
fDate
28-30 July 2015
Firstpage
877
Lastpage
882
Abstract
This paper presents a new attitude controller design method for underactuated reentry vehicles. Inverse dynamic method can´t be applied to a non-minimum phase system directly, while non-minimum phase problem is inevitable for underactuated reentry vehicles. In order to adopt inverse dynamic method to design attitude controller, a decomposition approach is introduced to cope with the non-minimum phase problem. In this approach, the normal form of 6-DOF equation of motion is deduced. Based on the normal form, the system is divided into two subsystems: a minimum phase one and a non-minimum phase one. And the dynamic equation of the internal dynamics can be obtained. Then the internal dynamics is stabilized with LQR method. Finally, the inverse dynamic controller can be obtained to stabilize the attitude of underactuated vehicle since the non-minimum phase problem is solved by the decomposition method beforehand. Simulation results demonstrate that the stabilization of the internal dynamics is guaranteed and the stable attitude control of underactuated reentry vehicle is also accomplished.
Keywords
Aerodynamics; Attitude control; Mathematical model; Symmetric matrices; Vehicle dynamics; Vehicles; LQR; attitude control; decomposition; dynamic inversion; non-minimum phase; underactuated reentry vehicle;
fLanguage
English
Publisher
ieee
Conference_Titel
Control Conference (CCC), 2015 34th Chinese
Conference_Location
Hangzhou, China
Type
conf
DOI
10.1109/ChiCC.2015.7259750
Filename
7259750
Link To Document