Nonlinear attitude control for a rigid spacecraft by feedback linearization
暂无分享,去创建一个
[1] Bong Wie,et al. Quaternion feedback for spacecraft large angle maneuvers , 1985 .
[2] Wan-Ho Jeon,et al. Aeroacoustic characteristics and noise reduction of a centrifugal fan for a vacuum cleaner , 2004 .
[3] Pramod P. Khargonekar,et al. Stability analysis of a missile control system with a dynamic inversion controller , 1998, Proceedings of the 1998 American Control Conference. ACC (IEEE Cat. No.98CH36207).
[4] John L. Crassidis,et al. Sliding Mode Control Using Modified Rodrigues Parameters , 1996 .
[5] Ching-Fang Lin,et al. Advanced Control Systems Design , 1993 .
[6] Hazem Ali Attia,et al. A computer method for the dynamic analysis of a system of rigid bodies in plane motion , 2004 .
[7] Pramod P. Khargonekar,et al. Stability Analysis of a Missile Control System with a Dynamic Inversion Controller , 1998 .
[8] Haim Weiss,et al. Quarternion feedback regulator for spacecraft eigenaxis rotations , 1989 .
[9] S. Vadali. Variable-Structure Control of Spacecraft Large-Angle Maneuvers , 1986 .
[10] Jianbo Lu,et al. Feedback control logic for spacecraft eigenaxis rotations under slew rate and control constraints , 1994 .