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Volumn 27, Issue 3, 2004, Pages 509-511

Extended kalman filtering for satellite orbital attitude estimation based on Gibbs vector

Author keywords

[No Author keywords available]

Indexed keywords

ALGORITHMS; COSINE TRANSFORMS; DIFFERENTIAL EQUATIONS; GAUSSIAN NOISE (ELECTRONIC); KALMAN FILTERING; KINEMATICS; ORBITS; REAL TIME SYSTEMS; SENSORS; STATISTICAL METHODS; WHITE NOISE;

EID: 2642584913     PISSN: 07315090     EISSN: 15333884     Source Type: Journal    
DOI: 10.2514/1.10338     Document Type: Article
Times cited : (9)

References (11)
  • 1
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    • Beijing Univ. of Aeronautics and Astronautics Press, Beijing, China
    • Zhang RenWei, Satellite Orbital Attitude Dynamics and Control, Beijing Univ. of Aeronautics and Astronautics Press, Beijing, China, 1998, pp. 137-222.
    • (1998) Satellite Orbital Attitude Dynamics and Control , pp. 137-222
    • Zhang, R.1
  • 2
    • 0030660848 scopus 로고    scopus 로고
    • Description of the milstar attitude determination system
    • American Automatic Control Council
    • Reid, D. B., "Description of the Milstar Attitude Determination System," Proceedings of the American Control Conference, Vol. 4, American Automatic Control Council, 1997, pp. 2313-2322.
    • (1997) Proceedings of the American Control Conference , vol.4 , pp. 2313-2322
    • Reid, D.B.1
  • 4
    • 0039185262 scopus 로고    scopus 로고
    • An attitude determination algorithm for a spacecraft using nonlinear filter
    • Yoon, Y. J., Choi, J. W., Lee, J. G., and Fang, T. H., "An Attitude Determination Algorithm for a Spacecraft Using Nonlinear Filter," KSME International Journal, Vol. 13, No. 2, 1999, pp. 130-143.
    • (1999) KSME International Journal , vol.13 , Issue.2 , pp. 130-143
    • Yoon, Y.J.1    Choi, J.W.2    Lee, J.G.3    Fang, T.H.4
  • 5
    • 0030126213 scopus 로고    scopus 로고
    • Estimation of rodrigues parameters from vector observations
    • Idan, M., "Estimation of Rodrigues Parameters from Vector Observations," IEEE Transactions on Aerospace and Electronic Systems, Vol. 32, No. 2, 1996, pp. 578-585.
    • (1996) IEEE Transactions on Aerospace and Electronic Systems , vol.32 , Issue.2 , pp. 578-585
    • Idan, M.1
  • 6
    • 0023306295 scopus 로고
    • Recursive attitude determination from vector observations: Euler angle estimation
    • Bar-Itzhack, I. Y., and Idan, M., "Recursive Attitude Determination from Vector Observations: Euler Angle Estimation," Journal of Guidance, Control, and Dynamics, Vol. 10, No. 2, 1987, pp. 152-157.
    • (1987) Journal of Guidance, Control, and Dynamics , vol.10 , Issue.2 , pp. 152-157
    • Bar-Itzhack, I.Y.1    Idan, M.2
  • 7
    • 0027685324 scopus 로고
    • A survey of attitude representations
    • Shuster, M. D., "A Survey of Attitude Representations," Journal of the Astronautical Sciences, Vol. 41, No. 4, 1993, pp. 437-517.
    • (1993) Journal of the Astronautical Sciences , vol.41 , Issue.4 , pp. 437-517
    • Shuster, M.D.1
  • 9
    • 0019384696 scopus 로고
    • Three-axis attitude determination from vector observations
    • Shuster, M. D., and Oh, S. D., "Three-Axis Attitude Determination from Vector Observations," Journal of Guidance and Control, Vol. 4, No. 1, 1981, pp. 70-77.
    • (1981) Journal of Guidance and Control , vol.4 , Issue.1 , pp. 70-77
    • Shuster, M.D.1    Oh, S.D.2
  • 10
    • 2642551913 scopus 로고    scopus 로고
    • Star-sensor-based predictive kalman filter for satellite attitude estimation
    • Lin, Y., and Deng, Z., "Star-Sensor-Based Predictive Kalman Filter for Satellite Attitude Estimation," Science in China (Series F), Vol. 45, No. 3, 2002, pp. 189-195.
    • (2002) Science in China (Series F) , vol.45 , Issue.3 , pp. 189-195
    • Lin, Y.1    Deng, Z.2
  • 11
    • 0025488733 scopus 로고
    • Kalman filtering of spacecraft attitude and the QUEST model
    • Shuster, M. D., "Kalman Filtering of Spacecraft Attitude and the QUEST Model," Journal of the Astronautical Sciences, Vol. 38, No. 3, 1990, pp. 377-393.
    • (1990) Journal of the Astronautical Sciences , vol.38 , Issue.3 , pp. 377-393
    • Shuster, M.D.1


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