DocumentCode
1919943
Title
Covariance analysis of spacecraft attitude control system
Author
Kim, Yoon-Hwan ; Park, Yonmook ; Bang, Hyochoong ; Tahk, Min-Jea
Volume
1
fYear
2003
fDate
23-25 June 2003
Firstpage
480
Abstract
The covariance analysis is applied to the performance of spacecraft attitude control systems. Subsystem considered here are the spacecraft bus, attitude controller, reaction wheel assembly, star-tracker unit, inertial reference unit, and gyro drift estimator. The results computed by the covariance analysis are compared with the results computed by the Monte-Carlo simulation. The covariance analysis is shown to be useful for studying the effects of system parameters on attitude control performance.
Keywords
attitude control; covariance analysis; gyroscopes; inertial navigation; nonlinear control systems; space vehicles; Monte-Carlo simulation; attitude controller; covariance analysis; gyro drift estimator; inertial reference unit; reaction wheel assembly; spacecraft attitude control system; spacecraft bus; star-tracker unit; system parameters; Acceleration; Angular velocity; Attitude control; Control system synthesis; Control systems; Equations; Performance analysis; Space vehicles; Torque; Wheels;
fLanguage
English
Publisher
ieee
Conference_Titel
Control Applications, 2003. CCA 2003. Proceedings of 2003 IEEE Conference on
Print_ISBN
0-7803-7729-X
Type
conf
DOI
10.1109/CCA.2003.1223462
Filename
1223462
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