Abstract:
We present new results on optimizing and dynamic synthesis of the nonlinear gyromoment attitude control systems for a fast-manoeuvring remote sensing spacecraft with a mi...Show MoreMetadata
Abstract:
We present new results on optimizing and dynamic synthesis of the nonlinear gyromoment attitude control systems for a fast-manoeuvring remote sensing spacecraft with a minimum-excessive scheme of single gimbal control moment gyroscopes, achieved by the exact feedback linearization and vector Lyapunov functions (VLF).
Published in: 1996 IEEE International Conference on Systems, Man and Cybernetics. Information Intelligence and Systems (Cat. No.96CH35929)
Date of Conference: 14-17 October 1996
Date Added to IEEE Xplore: 06 August 2002
Print ISBN:0-7803-3280-6
Print ISSN: 1062-922X