Velocity-free controllers for spacecraft attitude regulation: some further applications and results
暂无分享,去创建一个
[1] Amit Ailon,et al. A simple output-based stabilizing controller for attitude regulation of a rigid spacecraft with gas-jet actuators , 2001, Proceedings of the 2001 American Control Conference. (Cat. No.01CH37148).
[2] Jean-Jacques E. Slotine,et al. Hamiltonian adaptive control of spacecraft , 1990 .
[3] J. Wen,et al. Attitude control without angular velocity measurement: a passivity approach , 1996, IEEE Trans. Autom. Control..
[4] Henk Nijmeijer,et al. Global regulation of robots using only position measurements , 1993 .
[5] Romeo Ortega,et al. Global regulation of flexible joint robots using approximate differentiation , 1994 .
[6] James R. Wertz,et al. Spacecraft attitude determination and control , 1978 .
[7] Amit Ailon. Output controllers based on iterative schemes for set-point regulation of uncertain flexible-joint robot models , 1996, Autom..
[8] Sahjendra N. Singh,et al. Exact feedback linearization and control of space station using CMG , 1993, IEEE Trans. Autom. Control..
[9] T. Mori. Criteria for asymptotic stability of linear time-delay systems , 1985, IEEE Transactions on Automatic Control.
[10] Romeo Ortega,et al. An observer-based set-point controller for robot manipulators with flexible joints , 1993 .
[11] P. Crouch,et al. Spacecraft attitude control and stabilization: Applications of geometric control theory to rigid body models , 1984 .
[12] Amit Ailon,et al. Stability analysis of a rigid robot with output-based controller and time delay , 2000 .
[13] S. Skaar,et al. Arbitrary large-angle satellite attitude maneuvers using an optimal reaction wheel power criterion , 1982 .
[14] Panagiotis Tsiotras. Further passivity results for the attitude control problem , 1998, IEEE Trans. Autom. Control..
[15] V. Kolmanovskii,et al. Applied Theory of Functional Differential Equations , 1992 .
[16] Sahjendra N. Singh. Attitude control of a three rotor gyrostat in the presence of uncertainty , 1987 .
[17] Bong Wie,et al. New approach to attitude/momentum control for the Space Station , 1989 .