Sequential attitude and attitude-rate estimation using integrated-rate parameters

Journal of Guidance, Control, and Dynamics

Volumn 22, Issue 3, 1999, Pages 385-394

  Oshman, Yaakov ^a   Markley, F Landis ^b  

^a TECHNION ISRAEL INSTITUTE OF TECHNOLOGY   (Israel)

^b NASA GODDARD SPACE FLIGHT CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ACCELERATION; ALGORITHMS; COMPUTATIONAL COMPLEXITY; KINEMATICS; MATRIX ALGEBRA; RANDOM PROCESSES; SATELLITES; TRACKING (POSITION); VECTORS;

ANGULAR ACCELERATION; MAGNETOSPHERIC PARTICLE EXPLORER SPACECRAFT; SEQUENTIAL NONLINEAR ALGORITHM;

PARAMETER ESTIMATION;

EID: 0032630923     PISSN: 07315090     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.4404     Document Type: Article

References (28)

1. Lefferts, E. J., Markley, F. L., and Shuster, M. D., "Kalman Filtering for Spacecraft Attitude Estimation," Journal of Guidance, Control, and Dynamics, Vol. 5, No. 5, 1982, pp. 417-429.
2. Kudva, P., and Throckmorton, A., "Attitude Determination Studies for the Earth Observation System AMI (EOS-AM1) Mission," Journal of Guidance, Control, and Dynamics, Vol. 19, No. 6, 1996, pp. 1326-1331.
3. Flatley, T. W., Forden, J. K., Henretty, D. A., Lightsey, E. G., and Markley, F. L., "On-Board Attitude Determination and Control Algorithms for SAMPEX," Proceedings of Flight Mechanics/Estimation Theory Symposium, NASA CP 3102, NASA Goddard Space Flight Center, Greenbelt, MD, 1990, pp. 379-398.
4. Chu, D., Glickman, J., and Harvie, E., "Improvements in ERBS Attitude Determination Without Gyros," Proceedings of Flight Mechanics/Estimation Theory Symposium, NASA CP 3186, NASA Goddard Space Flight Center, Greenbelt, MD, 1992, pp. 185-200.
5. 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, No. 5, 1985, pp. 560-565.
6. Challa, M. S., Natanson, G. A., Baker, D. F., and Deutschmann, J. K., "Advantages of Estimating Rate Corrections During Dynamic Propagation of Spacecraft Rates - Applications to Real-Time Attitude Determination of SAMPEX," Proceedings of Flight Mechanics/Estimation Theory Symposium, NASA CP 3265, NASA Goddard Space Flight Center, Greenbelt, MD, 1994, pp. 481-495.
7. Azor, R., Bar-Itzhack, I. Y., and Harman, R. H., "Satellite Angular Rate Estimation from Vector Measurements," Journal of Guidance, Control, and Dynamics, Vol. 21, No. 3, 1998, pp. 450-457.
8. Algrain, M. C., and Saniie, J., "Interlaced Kalman Filtering of 3-D Angular Motion Based on Euler's Nonlinear Equations," IEEE Transactions on Aerospace and Electronic Systems, Vol. 30, No. 1, 1994, pp. 175-185.
9. Crassidis, J. L., and Markley, F. L., "Predictive Filtering for Attitude Estimation Without Rate Sensors," Journal of Guidance, Control, and Dynamics, Vol. 20, No. 3, 1997, pp. 522-527.
10. Lefferts, E. J., and Markley, F. L., "Dynamic Modeling for Attitude Determination," AIAA Paper 76-1910, Aug. 1976.
11. Mook, D. J., De Pena, J., Crassidis, J. L., and Meyer, T. J., "Dynamics-Based Robust Attitude Estimation," Proceedings of the AAS/AIAA Astrodynamics Specialist Conference (Victoria, BC, Canada), American Astronautical Society, San Diego, CA, 1993, pp. 39-58; also American Astronautical Society Paper 93-554, Aug. 1993.
12. Psiaki, M. L., Martel, F., and Pal, P. K., "Three Axis Attitude Determination via Kalman Filtering of Magnetometer Data," Journal of Guidance, Control, and Dynamics, Vol. 13, No. 3, 1990, pp. 506-514.
13. Ronen, M., and Oshman, Y., "A Third-Order, Minimal-Parameter Solution of the Orthogonal Matrix Differential Equation," Journal of Guidance, Control, and Dynamics, Vol. 20, No. 3, 1997, pp. 516-521.
14. Singer, R. A., "Estimating Optimal Tracking Filter Performance for Manned Maneuvering Targets," IEEE Transactions on Aerospace and Electronic Systems, Vol. AES-6, No. 4, 1970, pp. 473-483.
15. Wertz, J. R. (ed.), Spacecraft Attitude Determination and Control, D. Reidel, Dordrecht, The Netherlands, 1978, Chap. 13.
16. Oshman, Y., and Markley, F. L., "Minimal-Parameter Attitude Matrix Estimation from Vector Observations," Journal of Guidance, Control, and Dynamics, Vol. 21, No. 4, 1998, pp. 595-602.
17. 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), AIAA, Reston, VA, 1996, pp. 544-553 (AIAA Paper 96-3630).
18. Oshman, Y., and Bar-Itzhack, I. Y., "Eigenfactor Solution of the Matrix Riccati Equation - A Continuous Square Root Algorithm," IEEE Transactions on Automatic Control, Vol. AC-30, No. 10, 1985, pp. 971-978.
19. Chang, C. B., and Tabaczynski, J. A., "Application of State Estimation to Target Tracking," IEEE Transactions on Automatic Control, Vol. AC-29, No. 2, 1984, pp. 98-109.
20. ZhOu, H., and Kumar, K. S. P., "A 'Current' Statistical Model and Adaptive Algorithm for Estimating Maneuvering Targets," Journal of Guidance, Control, and Dynamics, Vol. 7, No. 5, 1984, pp. 596-602.
21. Mazor, E., Averbuch, A., Bar-Shalom, Y., and Dayan, J., "Interacting Multiple Model Methods in Target Tracking: A Survey," IEEE Transactions on Aerospace and Electronic Systems, Vol. 34, No. 1, 1998, pp. 103-123.
22. Maybeck, P. S., Stochastic Models, Estimation and Control, Vol. 1, Academic, New York, 1979, pp. 334-336.
23. Markley, F. L., "Attitude Determination Using Vector Observations and the Singular Value Decomposition," Journal of the Astronautical Sciences, Vol. 36, No. 3, 1988, pp. 245-258.
24. Bar-Itzhack, I. Y., and Meyer, J., "On the Convergence of Iterative Orthogonalization Processes," IEEE Transactions on Aerospace and Electronic Systems, Vol. AES-12, No. 2, 1976, pp. 146-151.
25. Mortari, D., Pollock, T. C., and Junkins, J. L., "Towards the Most Accurate Attitude Determination System Using Star Trackers," 8th AAS/AIAA Space Flight Mechanics Meeting, American Astronautical Society Paper 98-159, Monterey, CA, 1998.
26. Markley, F. L., "Attitude Determination Using Vector Observations: A Fast Optimal Matrix Algorithm," Journal of the Astronautical Sciences, Vol. 41,No. 2, 1993, pp. 261-280.
27. Black, H. D., "A Passive System for Determining the Attitude of a Satellite," AIAA Journal. Vol. 2, No. 7, 1964, pp. 1350, 1351.
28. Oshman, Y., and Markley, F. L., "Sequential Gyroless Attitude/Attitude-Rate Estimation Using Integrated-Rate Parameters," AIAA Paper 98-4508, Aug. 1998.