Nonlinear Observability Analysis of Spacecraft Attitude and Angular Rate with Inertia Uncertainty

Author:

Carmi Avishy,Oshman Yaakov

Publisher

Springer Science and Business Media LLC

Subject

Space and Planetary Science,Aerospace Engineering

Reference16 articles.

1. Gai, E., Daly, K., Harrison, J., and Lemos, L. “Star-Sensor-Based Satellite Attitude/Attitude Rate Estimator,” Journal of Guidance, Control, and Dynamics, Vol. 8, Sept.–Oct. 1985, pp. 560–565.

2. Challa, M.S., Natanson, G.A., Deutschmann, J.K., and Galal, K. “APC-Based Magnetometer-Only Attitude and Rate Determination System for Gyroless Spacecraft,” Proceedings of Flight Mechanics/Estimation Theory Symposium, NASA Goddard Space Flight Center, Greenbelt, MD, May 1995, NASA Conference Publication 3299, pp. 83–96.

3. Challa, M., Natanson, G., and Wheeler, C. “Simultaneous Determination of Spacecraft Attitude and Rates Using Only a Magnetometer,” Proceedings of the AIAA/AAS Astrodynamics Specialist Conference, San Diego, CA, July 1996.

4. Natanson, G. A., Challa, M.S., Deutschmann, J.K., and Baker, D.F. “Magnetometer-Only Attitude and Rate Determination for a Gyroless Spacecraft,” Proceedings of the Third International Symposium on Space Mission Operations and Ground Data Systems, NASA Goddard Space Flight Center, Greenbelt, MD, November 1994, NASA Conference Publication 3281, pp. 791–798.

5. Bar-Itzhack, I.Y., Harman, R.R., and Choukroun, D. “State-Dependent Pseudo Linear Filters for Spacecraft Attitude and Rate Estimation,” Proceedings of the AIAA Guidance, Navigation, and Control Conference, Monterey, California, Aug. 2002.

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