Parameter identification for the international space station using nonlinear momentum management control

1997 Guidance, Navigation, and Control Conference

Volumn , Issue , 1997, Pages 252-262

  Carter, Michael T ^a   Vadali, Srinivas R ^a   Chamitoff, Gregory E ^b  

^a Texas AandM University   (United States)

^b NASA JOHNSON SPACE CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMIC DRAG; AERODYNAMICS; ALGORITHMS; DRAG; INDUSTRIAL MANAGEMENT; SPACE STATIONS; SPACECRAFT;

AERODYNAMIC PARAMETERS; ATTITUDE MEASUREMENT; CENTER OF PRESSURE; INTERNATIONAL SPACE STATIONS; LYAPUNOV STABILITY THEORY; RECURSIVE LEAST-SQUARES IDENTIFICATIONS; ROTATIONAL DYNAMICS; SPACECRAFT ATTITUDE;

PARAMETER ESTIMATION;

EID: 33645265502     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (9)

1. Wie, B., Byun, K.W., Warren, V. W., Geller, D., Long, D., and Sunkel, J., “New Approach to Attitude/Momentum Control for the Space Station”, Journal of Guidance, Control, and Dynamics, Vol. 12, No. 5, 1989, pp. 714-722.
2. Warren, W.V., Wie, B., and Geller, D., “Periodic-Disturbance Accomodating Control of the Space Station for Asymptotic Momentum Management”, Journal of Guidance, Control, and Dynamics, Vol. 13, No. 6, 1990, pp. 984-992.
3. Harduvel, John T., “Continuous Momentum Management of Earth-Oriented Spacecraft”, Journal of Guidance, Control, and Dynamics, Vol. 15, No. 6, 1992, pp. 1417-1426.
4. Vadali, S.R., Oh, H.-S., “Space Station Attitude Control and Momentum Management: A Nonlinear Look”, Journal of Guidance, Control, and Dynamics, Vol. 15, No. 3, 1992, pp. 577-586.
5. Parlos, A.G., Sunkel, J.W., “Adaptive Attitude Control and Momentum Management for Large- Angle Spacecraft Maneuvers”, Journal of Guidance, Control, and Dynamics, Vol. 15, No. 4, 1992, pp.1018-1028.
6. Byun, K.-W., Wie, B., Geller, D., Sunkel, J., “Robust H∞ Control Design for the Space Station with Structured Parameter Uncertainty”, Journal of Guidance, Vol. 14, No. 6, 1991, pp. 1115-1122.
7. Cristi, R., Burl, J., Russo, N., “Adaptive Quaternion Feedback Regulation for Eigenaxis Rotations”, Journal of Guidance, Control, and Dynamics, Vol. 17, No. 6, 1994, pp. 1287-1291.
8. International Space Station On-Orbit Assembly, Modeling, and Mass Properties Databook: Design Analysis Cycle #2 Assembly Sequence, LESC-31166, Rev. D, Lockheed Engineering & Sciences, Co., May 1995.
9. Hughes, P.C., Spacecraft Attitude Dynamics, John Wiley & Sons, New York, 1986, pp. 293-298.