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Chapter 8 - Momentum-Biased Attitude Stabilization

Published online by Cambridge University Press:  18 December 2014

Marcel J. Sidi
Affiliation:
Israel Aircraft Industries Ltd
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Chapter
Information
Spacecraft Dynamics and Control
A Practical Engineering Approach
, pp. 210 - 259
Publisher: Cambridge University Press
Print publication year: 1997

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References

Agrawal, B. N. (1986), Design of Geosynchronous Spacecraft. Englewood Cliffs, NJ: Prentice-Hall.Google Scholar
Azor, R. (1992), “Solar Attitude Control Including Active Denutation Damping in a Fixed Momentum Wheel Satellite,” AIAA Guidance Navigation and Control Conference (10–12 August, Hilton Head Island, SC). Washington, DC: AIAA, pp. 226–35.
Azor, R. (1995), “Roll/Yaw Attitude Control and Denutation by Thrusters,” Israel Annual Conference on Aviation and Astronautics (February, Tel Aviv). Tel Aviv: Kenes, pp.86–94.
Benoit, A., and Bailly, M. (1987), “In-Orbit Experience Gained with the European OTS/ECS/TELECOM 1 Series of Spacecraft” (AAS 87-054), Proceedings of the Annual Rocky Mountain Guidance and Control Conference (31 January - 4 February 1987, Keystone, CO). San Diego, CA: American Astronautical Society, pp.525–42.Google Scholar
Bingham, N., Craig, A., and Flook, L. (1984), “Evolution of European Telecommunication Satellite Pointing Performance,” Paper no. 84-0725, AIAA, New York.
Bittner, H., Bruderle, E., Roche, Ch., and Schmidts, W. (1977), “The Attitude Determination and Control Subsystem of the Intelsat V Spacecraft” (ESA SP-12), Proceedings of AOCS Conference (3–6 October, Noordwijk, Netherlands). Paris: European Space Agency.Google Scholar
Bryson, A. (1983), “Stabilization and Control of Spacecraft,” Microfiche supplement to the Proceedings of the Annual AAS Rocky Mountain Guidance and Control Conference (5-9 February, Keystone, CO). San Diego, CA: American Astronautical Society.Google Scholar
Devey, W. J., Field, C. F., and Flook, L. (1977), “An Active Nutation Control System for Spin Stabilized Satellites”Automatica 13:161–72.CrossRefGoogle Scholar
Dougherty, H. J., Lebsock, K. L., and Rodden, J. J. (1971), “Attitude Stabilization of Synchronous Communications Satellite Employing Narrow-Beam Antennas,”Journal of Spacecraft and Rockets 8: 834–41.CrossRefGoogle Scholar
Dougherty, H. J., Scott, E. D., and Rodden, J. J. (1968), “Analysis and Design of WHECON - An Attitude Control Concept,” Paper no. 68-461, AIAA 2nd Communications Satellite Systems Conference (8-10 April, San Francisco).CrossRefGoogle Scholar
Duhamel, T., and Benoit, A. (1991), “New AOCS Concepts for ARTEMIS and DRS,”Space Guidance, Navigation and Control Systems (Proceedings of the First EAS International Conference, ESTEC, 4-7 June, Noordwijk, Netherlands). Paris: European Space Agency, pp. 33–9.Google Scholar
Forward, R. L. (1990), “Grey Solar Sails,”Journal of the Astronautical Sciences 38(2): 161–85.Google Scholar
Fox, S. (1986), “Attitude Control Subsystem Performance of the RCA Series 3000 Satellite,” Paper no. 86-0614-CP, AIAA 11th Communications Satellite System Conference (17-20 March, San Diego, CA).
Georgevic, R. M. (1973), “The Solar Radiation Pressure Force and Torques Model,”Journal of the Astronautical Sciences 20(5): 257–74.Google Scholar
Iwens, R. P., Fleming, A. W., and Spector, V. A. (1974), “Precision Attitude Control with a Single Body-Fixed Momentum Wheel,” Paper no. 74-894, AIAA Mechanics and Control of Flight Conference (5-9 August, Anaheim, CA).
Lebsock, K. L. (1980), “High Pointing Accuracy with a Momentum Bias Attitude Control System,”Journal of Guidance and Control 3(3): 195–202.CrossRefGoogle Scholar
Lebsock, K. L. (1982), “Magnetic Desaturation of a Momentum Bias System,” Paper no. 82-1468, AIAA/AAS Astrodynamics Conference (9-11 August, San Diego, CA).
Lievre, J. (1985), “Solar Sailing Attitude Control of Large Geostationary Satellite,”IFAC Automatic Control in Space. Oxford, UK: Pergamon, pp. 29–33.Google Scholar
Maute, P., Blancke, B., Jahier, J., and Alby, F. (1989), “Autonomous Geostationary Stationkeeping System Optimization and Validation,”Acta Automatica 20: 93–101.Google Scholar
Muhlfelder, L. (1984), “Attitude Control System Evolution of Body-Stabilized Communication Spacecraft,” Paper no. 84-1839, AIAA Guidance and Control Conference (20-22 August, Seattle). Washington, DC: AIAA, pp. 55–62.Google Scholar
Phillips, K. (1973), “Active Nutation Damping Utilizing Spacecraft Mass Properties,”IEEE Transactions on Aerospace and Electronic Systems 9(5): 688–93.Google Scholar
Renner, U. (1979), “Attitude Control by Solar Sailing - A Promising Experiment with OTS-2,”ESA Journal 3(1): 35–40.Google Scholar
Schmidt, G. E. (1975), “The Application of Magnetic Attitude Control to a Momentum-Biased Synchronous Communication Satellite,” Paper no. 75-1055, AIAA Guidance and Control Conference (20-22 August, Boston).
Schmidt, G. E., and Mulhfelder, L. (1981), “The Application of Magnetic Torquing to Spacecraft Attitude Control” (AAS 81-002), Proceedings of the Annual Rocky Mountain Guidance and Control Conference (31 January - 4 February, Keystone, CO). San Diego, CA: American Astronautical Society.Google Scholar
Sidi, M. (1992a), “Attitude Stabilization of Bias-Momentum Satellites,” Israel Annual Conference on Aviation and Astronautics (18-20 February, Tel Aviv). Tel Aviv: Kenes, pp. 333–8.
Sidi, M. (1992b), “Reactive Thrust Cruise for a Geosynchronous Bias-Momentum Satellite with Active Denutation,” 12th FAC Symposium in Aerospace Control (7-11 September, Ottobrunn, Germany). Oxford, UK: Pergamon, pp. 201–5.
Wertz, J. R. (1978), Spacecraft Attitude Determination and Control. Dordrecht: Reidel.CrossRefGoogle Scholar
Wie, B., Lehner, J., and Plescia, C. (1985), “Roll/Yaw Control of Flexible Spacecraft Using Skewed Bias Momentum Wheels,”Journal of Guidance, Control, and Dynamics 8(4): 447–51.CrossRefGoogle Scholar

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