DocumentCode :
234353
Title :
Steering law design with perturbed Jacobian matrix for Single Gimbal Control Moment Gyroscopes
Author :
Zhong Wu ; Zhen Wang ; Shilong Deng ; Ruidong Yan
Author_Institution :
Sch. of Instrum. Sci. & Optoelectron. Eng., Beihang Univ., Beijing, China
fYear :
2014
fDate :
28-30 July 2014
Firstpage :
2271
Lastpage :
2275
Abstract :
Steering law design for Single Gimbal Control Moment Gyroscopes (SGCMGs) can be transformed into a problem of nonlinear programming with nonsingular constraint. Although the suboptimal solution to the nonlinear programming has the closed form through the estimation of the Kuhn-Tucker multipliers without sophisticated numerical calculations, it is still often trapped in the elliptic singular points. In this paper, a modified steering law based on nonlinear programming is presented. In this algorithm, a proper gimbal perturbation is inserted into the Jacobian matrix actively when SGCMGs are approaching to or locked in the singular points. Thus, the algorithm can output feasible gimbal commands even near singularities and can force the gimbals leave singular configurations for the desired ones. Extensive simulation results demonstrate the effectiveness of the proposed method.
Keywords :
Jacobian matrices; control system synthesis; gyroscopes; nonlinear programming; Kuhn-Tucker multipliers; SGCMG; elliptic singular points; gimbal commands; nonlinear programming; nonsingular constraint; perturbed Jacobian matrix; single gimbal control moment gyroscopes; singular gyroscope configurations; steering law design; Aerodynamics; Attitude control; Gyroscopes; Jacobian matrices; Programming; Space vehicles; Torque; Attitude Control; Control Moment Gyroscopes; Spacecraft; Steering Law;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Control Conference (CCC), 2014 33rd Chinese
Conference_Location :
Nanjing
Type :
conf
DOI :
10.1109/ChiCC.2014.6896986
Filename :
6896986
Link To Document :
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