Azor, R. (1993), “Momentum Management and Torque Distribution in a Satellite with Reaction Wheels,” Israel Annual Conference on Aviation and Astronautics (24–25 February, Tel Aviv). Tel Aviv: Kenes, pp. 339–47.

Bikdash, M., Cliff, E., and Nayfeh, A. (1993), “Saturating and Time Optimal Feedback Controls,”Journal of Guidance, Control, and Dynamics 16(3): 541–8.CrossRefGoogle Scholar

Bilimora, K., and Wie, B. (1993), “Time-Optimal Three-Axis Reorientation of a Rigid Spacecraft,”Journal of Guidance, Control, and Dynamics 16(3): 446–60.Google Scholar

Bollner, M. (1991), “On-board Control System Performance of the Rosat Spacecraft,”Acta Astronautica 25(8/9): 487–95.CrossRefGoogle Scholar

Boorg, P. (1982), “Validation for Spot Attitude Control System Development,”IFAC Automatic Control System Development.Noordwijk, Netherlands, pp. 67–73.

Bosgra, J. A., and Prins, M. J. (1982), “Testing and Investigation of Reaction Wheels,”IFAC Automatic Control in Space. Noordwijk, Netherlands, pp. 449–58.Google Scholar

Bosgra, J. A., and Smilde, H. (1982), “Experimental and Systems Study of Reaction Wheels. Part I: Measurement and Statistical Analysis of Forces and Torque Irregularities,”National Aerospace Laboratory, NLR, Netherlands.

Bryson, A., and Ho, Y. (1969), Applied Optimal Control. Waltham, MA: Blaisdel.Google Scholar

D'Azzo, J. J., and Houpis, C. H. (1988), Linear Control System Analysis and Design, Conventional and Modern. New York: McGraw-Hill.Google Scholar

Dorf, C. R. (1989), Modern Control Systems. 5th ed. Reading, MA: Addison-Wesley.Google Scholar

Dougherty, H., Rodoni, C., Tompetrini, K., and Nakashima, A. (1982), “Space Telescope Control,”IFAC Automatic Control in Space. Oxford, UK: Pergamon, pp. 15–24.Google Scholar

Elgerd, O. (1967), Control System Theory. New York: McGraw-Hill.Google Scholar

Fleming, A. W., and Ramos, A. (1979), “Precision Three-Axis Attitude Control via Skewed Reaction Wheel Momentum Management,” Paper no. 79-1719, AIAA Guidance and Control (6-8 August, Boulder, CO). New York: AIAA, pp. 177–90.

Glaese, J. R., Kennel, H. F., Nurre, G. S., Seltzer, S. M., and Shelton, H. L. (1976), “Low-Cost Space Telescope Pointing Control System,”Journal of Spacecraft and Rockets 13(7): 400–5.CrossRefGoogle Scholar

James, H. M., Nichols, N. B., and Phillips, R. S. (1955), Theory of Servomechanisms (MIT Radiation Laboratory Series, vol. 25). New York: McGraw-Hill.Google Scholar

Junkins, J. L., and Turner, J. D. (1986), Optimal Spacecraft Rotational Maneuvers. Amsterdam: Elsevier.Google Scholar

Kaplan, M. (1976), Modern Spacecraft Dynamics and Control. New York: Wiley.Google Scholar

Lebsock, K. (1982), “Magnetic Desaturation of a Momentum Bias System,” AIAA/AAS Astrodynamics Conference (9-11 August, San Diego). New York: AIAA.

McElvain, R. J. (1962), “Satellite Angular Momentum Removal Utilizing the Earth's Magnetic Field,” Space Systems Division, Hughes Aircraft Co., El Segundo, CA.

Oh, H. S., and Valadi, S. R. (1991), “Feedback Control and Steering Laws for Spacecraft Using Single Gimbal Control Moment Gyros,”Journal of the Astronautical Sciences 39(2): 183–203.Google Scholar

Pierre, A. D. (1986), Optimization Theory with Applications. New York: Dover.Google Scholar

Pircher, M. (1989), “Spot 1 Spacecraft in Orbit Performance,”IFAC Automatic Control in Space. Noordwijk, Netherlands.Google Scholar

Schletz, B. (1982), “Use of Quaternion in Shuttle Guidance,” Paper no. 82-1557, AIAA Conference on Navigation and Control (9–11 August, San Diego). New York: AIAA, pp. 753–60.

Solodovnikov, V. V. (1960), Introduction to the Statistical Dynamics of Automatic Control Systems. New York: Dover.Google Scholar

Stickler, A. C., and Alfriend, K. (1976), “Elementary Magnetic Attitude Control System,”Journal of Spacecraft and Rockets 13(5): 282–7.CrossRefGoogle Scholar

Wertz, J. R. (1986), Spacecraft Attitude Determination and Control. Dordrecht: Reidel.Google Scholar

Wie, B., Weiss, H., and Arapostathis, A. (1989), “Quaternion Feedback Regulator for Spacecraft Eigenaxis Rotations,”Journal of Guidance, Control, and Dynamics 12(3): 375–80.CrossRefGoogle Scholar