Nonlinear control and stability analysis of spacecraft attitude recovery
暂无分享,去创建一个
[1] E. L. Marsh,et al. The attitude control of a flexible solar electric spacecraft , 1970 .
[2] Rajni V. Patel,et al. Inversion-based sliding control of a flexible-link manipulator , 1998 .
[3] Yiing-Yuh Lin,et al. Non-linear control with Lyapunov stability applied to spacecraft with flexible structures , 2001 .
[4] A. Isidori. Nonlinear Control Systems , 1985 .
[5] Rajnikant V. Patel,et al. Nonlinear tip-position tracking control of a flexible-link manipulator: theory and experiments , 2001, Autom..
[6] Sahjendra N. Singh. Flexible spacecraft maneuver: Inverse attitude control and modal stabilization☆ , 1988 .
[7] S.N. Singh,et al. Feedback linearization and solar pressure satellite attitude control , 1996, IEEE Transactions on Aerospace and Electronic Systems.
[8] Suresh M. Joshi,et al. Control of Nonlinear Multibody Flexible Space Structures , 1996 .
[9] C. LaVigna,et al. Nonlinear and Adaptive Control of Flexible Space Structures , 1993 .
[10] Victor Larson,et al. Optimal Estimation and Attitude Control of a Solar Electric Propulsion Spacecraft , 1977, IEEE Transactions on Aerospace and Electronic Systems.
[11] R. Quinn,et al. Equations of motion for maneuvering flexible spacecraft , 1987 .
[12] S. Monaco,et al. A nonlinear attitude control law for a satellite with flexible appendages , 1985, 1985 24th IEEE Conference on Decision and Control.
[13] P. Grote,et al. Equations of Motion of Flexible Spacecraft , 1970 .
[14] Sahjendra N. Singh,et al. Feedback Linearization and Control of NASA SCOLE System by Output Feedback , 1991, 1991 American Control Conference.
[15] Sahjendra N. Singh. Nonlinear attitude control of flexible spacecraft under disturbance torque , 1986 .
[16] James R. Wertz,et al. Spacecraft attitude determination and control , 1978 .
[17] Siamak Tafazoli,et al. On Attitude Recovery of Spacecraft using Nonlinear Control , 2020, ArXiv.
[18] Yiing-Yuh Lin,et al. General attitude control and stability of spacecraft with flexible structures , 1999 .
[19] Sahjendra N. Singh,et al. Adaptive control and stabilization of elastic spacecraft , 1997 .
[20] J.S. Yuan,et al. Closed-loop manipulator control using quaternion feedback , 1988, IEEE J. Robotics Autom..
[21] Sahjendra Singh,et al. Nonlinear Adaptive Attitude Control of Spacecraft , 1987, IEEE Transactions on Aerospace and Electronic Systems.
[22] Sahjendra Singh,et al. Robust Nonlinear Attitude Control of Flexible Spacecraft , 1987, IEEE Transactions on Aerospace and Electronic Systems.
[23] J. Wen,et al. Robust attitude stabilization of spacecraft using nonlinear quaternion feedback , 1995, IEEE Trans. Autom. Control..
[24] G Maghami Peiman,et al. A Class of Stabilizing Controllers for Flexible Multibody Systems , 1995 .
[25] Wayne J. Book,et al. Controller Design for Flexible, Distributed Parameter Mechanical Arms Via Combined State Space and Frequency Domain Techniques , 1983 .
[26] S. Di Gennaro,et al. Output stabilization of flexible spacecraft with active vibration suppression , 2003 .
[27] B. Ickes. A new method for performing digital control system attitude computations using quaternions , 1970 .
[28] A. H. Gale,et al. Influence of Flexible Appendages on Dual-Spin Spacecraft Dynamics and Control , 1970 .
[29] Sahjendra N. Singh,et al. Sliding mode control of flexible spacecraft under disturbance torque , 1988, Proceedings of the 27th IEEE Conference on Decision and Control.
[30] Lawrence W. Taylor,et al. A mathematical problem and a Spacecraft Control Laboratory Experiment (SCOLE) used to evaluate control laws for flexible spacecraft. NASA/IEEE design challenge , 1984 .
[31] Gern Liang Lin,et al. Robust nonlinear attitude control of spacecraft with flexible structures , 2000 .