DocumentCode
3008915
Title
Finite-time stabilization of the NASA CEV reaction control system with actuator saturation and by position measurements
Author
Frye, Michael T. ; Li, Ji ; Qian, Chunjiang
Author_Institution
Dept. of Electr. Eng., Texas Univ., San Antonio, TX, USA
fYear
2004
fDate
38079
Firstpage
93
Lastpage
98
Abstract
This paper studies the problem of finite-time stabilization of planar systems whose control input is subjected to saturation caused by actuator limitations. Finite-time control deals with convergence within a finite settling time and therefore guarantees the performance of a nonlinear system within a specific time T. In the literature, most of the existing finite-time convergent controllers are unbounded and therefore are not implementable for a system with actuator saturation. In this paper, we propose a design method of the finite-time convergent controller which is bounded by a prior given bound. We show that the controller, together with a finite-time convergent observer, will effectively move the system to the origin in finite time. As an example of an application of our controller, we will apply our results on the NASA Crew Exploration Vehicle reaction control system thrusters to demonstrate the effectiveness of the proposed controller for use on a system with saturation constraints. Our results indicate that finite-time controllers would be an ideal candidate for use on the Crew Exploration Vehicle reaction control system thrusters.
Keywords
attitude control; closed loop systems; control nonlinearities; convergence; optimal control; redundancy; robust control; space vehicles; state feedback; NASA crew exploration vehicle; actuator limitations; actuator saturation; attitude control; closed-loop system; control system thrusters; convergence; design method; double integrator; dynamic compensator; finite settling time; finite-time stabilization; nonlinear system performance; observer; output feedback; planar systems; position measurements; reaction control system; redundant systems; state feedback controller; switching logic; Actuators; Atmosphere; Control systems; Convergence; Moon; NASA; Nonlinear control systems; Output feedback; Position measurement; Vehicles;
fLanguage
English
Publisher
ieee
Conference_Titel
Region 5 Conference: Annual Technical and Leadership Workshop, 2004
Print_ISBN
0-7803-8217-X
Type
conf
DOI
10.1109/REG5.2004.1300170
Filename
1300170
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