DocumentCode
55536
Title
Decoupling trajectory tracking for gliding reentry vehicles
Author
Zixuan Liang ; Zhang Ren ; Xingyue Shao
Author_Institution
Sci. & Technol. on Aircraft Control Lab., Beihang Univ., Beijing, China
Volume
2
Issue
1
fYear
2015
fDate
January 10 2015
Firstpage
115
Lastpage
120
Abstract
A decoupling trajectory tracking method for gliding reentry vehicles is presented to improve the reliability of the guidance system. Function relations between state variables and control variables are analyzed. To reduce the coupling between control channels, the multiple-input multiple-output (MIMO) tracking system is separated into a series of two single-input single-output (SISO) subsystems. Tracking laws for both velocity and altitude are designed based on the sliding mode control (SMC). The decoupling approach is verified by the Monte Carlo simulations, and compared with the linear quadratic regulator (LQR) approach in some specific conditions. Simulation results indicate that the decoupling approach owns a fast convergence speed and a strong anti-interference ability in the trajectory tracking.
Keywords
MIMO systems; Monte Carlo methods; aircraft control; linear quadratic control; trajectory control; variable structure systems; LQR approach; MIMO tracking system; Monte Carlo simulations; SISO subsystems; SMC; antiinterference ability; control variables; convergence speed; decoupling trajectory tracking method; function relations; gliding reentry vehicles; guidance system reliability; linear quadratic regulator approach; multiple-input multiple-output tracking system; single-input single-output subsystems; sliding mode control; state variables; Aerodynamics; Earth; MIMO; Mathematical model; Trajectory; Uncertainty; Vehicles; Hypersonic; decoupling control; reentry vehicle; sliding mode control (SMC); trajectory tracking;
fLanguage
English
Journal_Title
Automatica Sinica, IEEE/CAA Journal of
Publisher
ieee
ISSN
2329-9266
Type
jour
DOI
10.1109/JAS.2015.7032913
Filename
7032913
Link To Document