Satellite Attitude Control Using Only Electromagnetic Actuation
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[1] J. Cappellari,et al. Mathematical theory of the Goddard trajectory determination system , 1976 .
[2] Mogens Blanke,et al. Three-Axis Satellite Attitude Control Based on Magnetic Torquing , 1996 .
[3] Ward L. Ebert,et al. Autonomous spacecraft attitude control using magnetic torquing only , 1989 .
[4] Weiping Li,et al. Applied Nonlinear Control , 1991 .
[5] Rafal Wisniewski. Nonlinear Control for Satellite Detumbling Based on Magnetic Torquing , 1994 .
[6] Thomas Bak,et al. Autonomous attitude determination and control system for the Orsted satellite , 1996, 1996 IEEE Aerospace Applications Conference. Proceedings.
[7] Huibert Kwakernaak,et al. Linear Optimal Control Systems , 1972 .
[8] Frank L. Lewis,et al. Optimal Control , 1986 .
[9] J. Wen,et al. The attitude control problem , 1991 .
[10] James R. Wertz,et al. Spacecraft attitude determination and control , 1978 .
[11] Christopher I. Byrnes,et al. On the attitude stabilization of rigid spacecraft , 1991, Autom..
[12] W. Rudin. Real and complex analysis , 1968 .
[13] Vasile Mihai Popov,et al. Hyperstability of Control Systems , 1973 .
[14] C. A. Desoer,et al. Nonlinear Systems Analysis , 1978 .
[15] Vadim I. Utkin,et al. Sliding Modes in Control and Optimization , 1992, Communications and Control Engineering Series.
[16] A. Isidori. Nonlinear Control Systems , 1985 .
[17] Thomas Bak. Onboard Attitude Determination for a Small Satellite , 1996 .
[18] Paolo Nistri,et al. A Sliding Manifold Approach to Satellite Attitude Control , 1993 .
[19] S. Bittanti,et al. The Riccati equation , 1991 .
[20] Wolfgang Hahn,et al. Stability of Motion , 1967 .
[21] Cishen Zhang,et al. Performance Analysis of Periodically Time Varying Controllers , 1996 .
[22] Mark L. Psiaki,et al. N 8 9 - 1 5 9 5 1 Three-Axis Attitude Determination via Kalman Filtering of Magnetometer Data , 2003 .
[23] Giuseppe De Nicolao,et al. Cyclomonotonicity, riccati equations and periodic receding horizon control , 1994, Autom..