Time-Fuel Optimal Trajectory Based Attitude Maneuver Control for Flexible Spacecraft
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[1] Hyochoong Bang,et al. Maneuver and vibration control of hybrid coordinate systems using Lyapunov stability theory , 1993 .
[2] Jongrae Kim,et al. Engineering Notes Backstepping Control Design with Actuator Torque Bound for Spacecraft Attitude Maneuver , 2010 .
[3] Hu Qing-lei. Variable structure control with time-varying sliding mode and vibration control for flexible satellite , 2009 .
[4] Glenn Creamer. Attitude determination and control of Clementine during lunar mapping - Description and on-orbit performance , 1995 .
[5] R. C. Thompson,et al. Survey of time-optimal attitude maneuvers , 1994 .
[6] Youdan Kim,et al. Robust backstepping control for slew maneuver using nonlinear tracking function , 2003, IEEE Trans. Control. Syst. Technol..
[7] Lihua Xie,et al. Robust and adaptive variable structure output feedback control of uncertain systems with input nonlinearity , 2008, Autom..
[8] Per Johan Nicklasson,et al. Satellite attitude control by quaternion-based backstepping , 2005 .
[9] Qinglei Hu. Sliding mode maneuvering control and active vibration damping of three-axis stabilized flexible spacecraft with actuator dynamics , 2008 .
[10] M. Akella,et al. Globally stabilizing saturated attitude control in the presence of bounded unknown disturbances , 2005 .
[11] I. Michael Ross,et al. Spectral Algorithm for Pseudospectral Methods in Optimal Control , 2008, Journal of Guidance, Control, and Dynamics.
[12] Paul DeLaHunt,et al. ATTITUDE DETERMINATION AND CONTROL OF CLEMENTINE DURING LUNAR MAPPING , 1996 .
[13] Jyh-Ching Juang,et al. Spacecraft robust attitude tracking design: PID control approach , 2002, Proceedings of the 2002 American Control Conference (IEEE Cat. No.CH37301).