Magnetometer-only linear attitude estimation for bias momentum pico-satellite
Author:
Publisher
Zhejiang University Press
Subject
General Engineering
Link
http://link.springer.com/content/pdf/10.1631/jzus.A0900725.pdf
Reference21 articles.
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2. Bang, H., Kim, J.A., Kim, M., 1997. Optimal reorientation maneuver of bias momentum spacecraft. Journal of Guidance, Control and Dynamics, 20(6):1076–1082. [doi:10.2514/2.4188]
3. Challa, M., Natanson, G., Ottenstein, N., 2000. Magnetometer-only Attitude and Rate Estimates for Spinning Spacecraft. Proceedings of the AIAA/AAS Astrodynamics Specialists Conference, Denver, CO, USA, p.311–321.
4. Côté, J., Lafontaine, J., 2008. Magnetic-only Orbit and Attitude Estimation Using the Square-root Unscented Kalman Filter Application to the PROBA-2 Spacecraft, Guidance, Navigation and Control Conference and Exhibit, Honolulu, Hawaii, USA.
5. Crassidis, J.L., Lai, K.L., Harman, R.R., Real-time attitudeindependent three-axis magnetometer calibration. Journal of Guidance, Control, and Dynamics, 28(1):115–120. [doi:10.2514/1.6278]
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