Attitude determination for gyrostats in non-equilibrium spins from infrequent vector observations

AIAA Guidance, Navigation, and Control Conference and Exhibit

Volumn , Issue , 2000, Pages

  Peck, Mason A ^a  

^a BOEING COMPANY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ANGULAR MOMENTUM; ATTITUDE CONTROL; DIFFERENCE EQUATIONS; ENERGY DISSIPATION; NONLINEAR EQUATIONS; SPACECRAFT PROPULSION;

ANGULAR RATE MEASUREMENTS; ATTITUDE DETERMINATION; AUTO REGRESSIVE MODELS; MISSION OPERATIONS; PERFORMANCE INDICES; RECURSIVE LEAST SQUARES; SPINNING SPACECRAFTS; VECTOR OBSERVATIONS;

ORBITS;

EID: 85086494352     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2000-3946     Document Type: Conference Paper

References (13)

1. Wahba, Grace, "A Least-Squares Estimate of Spacecraft Attitude," SIAM Review, Vol. 7, No. 3, July 1965, p.409.
2. Farrell, J. L. and J. C. Stuelpnagel, "A Least Squares Estimate of Spacecraft Attitude," SIAM Review, Vol. 8, No. 3, July 1966, pp. 384-386.
3. Keat, J., "Analysis of Least-Squares Attitude Determination Routine DOAOP," CSC Report CSC/TM-77/6034, February 1977.
4. Lemer, Gerald M., "Three-Axis Attitude Determination," in Spacecraft Attitude Determination and Control, ed. by James R. Wertz, Dordrecht, Holland, D.Reidel, 1978.
5. Markley, F. Landis, "Attitude Determination Using Vector Observations and the Singular Value Decomposition," AAS Paper 87-490, AAS/AIAA Astrodynamics Specialist Conference, Kalispell, MT, August 1987.
6. Markley, F. Landis, "Attitude Determination Using Vector Observations: a Fast Optimal Matrix Algorithm," Journal of the Astronautical Sciences, Vol. 41, No. 2, April-June 1993, pp. 261-280.
7. Mortari, Daniele, "ESOQ: A Closed-Form Solution to the Wahba Problem," Journal of the Astronautical Sciences, Vol. 45, No. 2 April-June 1997, pp. 509-515.
8. Mortari, Daniele, "ESOQ2 Single-Point Algorithm for Fast Optimal Attitude Determination," Journal of Guidance, Control and Dynamics (in press).
9. Kaplan, Marshall H., Modern Spacecraft Dynamics and Control, New York, John Wiley & Sons, 1976.
10. Markley, F. Landis, "How to Estimate Attitude from Vector Observations," AAS Paper 99-427, AAS/AIAA Astrodynamics Specialist Conference, Girdwood, Alaska, August 1999.
11. Peck, Mason A., "Mass-Properties Identification for Spacecraft with Powerful Damping," AAS Paper 99-430, AAS/AIAA Astrodynamics Specialist Conference, Girdwood, Alaska, August 1999.
12. Ahmed, J., Coppola, V. T., and D. S. Bernstein, "Adaptive Asymptotic Tracking of Spacecraft Attitude Motion with Inertia Matrix Identification." AIAA Paper 97-3530, AIAA Guidance, Navigation, and Control Conference, New Orleans, LA, Aug. 11-13, 1997.
13. Hughes, P.: Spacecraft Attitude Dynamics, John Wiley & Sons, Toronto, Canada, 1986.