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
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