Modeling of non-redundant RCS system and hybrid control of high L/D gliding vehicle

Author

Shi Linan ; Li Huifeng ; Wang Zhi

Author_Institution

Sch. of Astronaut., Beijing Univ. of Aeronaut. & Astronaut., Beijing, China

fYear

2014

Firstpage

645

Lastpage

650

Abstract

Three degree-of-freedom model which describes the dynamics of unpowered gliding reentry vehicle is established. The output torques of RCS which described in body axis system and the control sequence of RCS are designed. Considering the station of low dynamic pressure, the hybrid control of reaction control system and aerodynamic control surfaces for gliding reentry vehicle was then designed. To solve the problem of control allocation, in the longitudinal control of vehicle, time-sharing control was adopted while hybrid control in the lateral control of vehicle. The simulation shows that the strategies and functions of control system are practical and the feasible of the hybrid control system.

Keywords

aerodynamics; aircraft control; position control; torque control; vehicle dynamics; RCS control sequence; RCS output torque; aerodynamic control surface; body axis system; control allocation; hybrid control system; lateral control; longitudinal control; nonredundant RCS system; reaction control system; three degree-of-freedom model; time-sharing control; unpowered gliding reentry vehicle; vehicle dynamics; Actuators; Aerodynamics; Attitude control; Vehicle dynamics; Vehicles; RCS; attitude control; hybrid control; hypersonic vehicles;

fLanguage

English

Publisher

ieee

Conference_Titel

Intelligent Control and Automation (WCICA), 2014 11th World Congress on

Type

conf

DOI

10.1109/WCICA.2014.7052790

Filename

7052790