Robust Output Feedback Attitude Control of Spacecraft Using Solar Radiation Pressure

Author:

Srinivasan Lakshmi,Lee Keum W.,Singh Sahjendra N.

Publisher

Springer International Publishing

Reference22 articles.

1. Alvarez-Ramirez,J.: Adaptive Control of Feedback Linearizable Systems: A Modeling Error Compensation Approach. Int. J. Robust Nonlin. Contr. 9 (1999) 361–377

2. Esfandiari, F., Khalil, H. K.: Output Feedback Stabilization of Fully Linearizable Systems. Int. J. Control. 56(5) (1992) 1007–1037

3. Joshi, V. K., Kumar, K.: New solar attitude control approach for satellites in elliptic orbits. J. Guidance, Control, and Dynamics. 3(1) (1980) 42–47

4. Khalil, H.K., Esfandiari,F.: Semiglobal Stabilization of a Class of Nonlinear Systems Using Output Feedback. IEEE Tr. Automat. Control. 38(9) (1993) 1412–1415

5. Lee, K.W., Singh, S.N.: Non-certainty-equivalent adaptive satellite attitude control using solar radiation pressure. Proc. IMechE. Part G: J. Aerospace Eng. 223 (2009) 977–988

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