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[2]
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[3]
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Meirovitch, Quinn, Maneuvering and vibration control of flexible spacecraft, J. Astronaut. Sci., 35, pp. 301-328, (1987)
[5]
Taylor, Balakrishnan, A mathematical problem and a Spacecraft Control Laboratory Experiment (SCOLE) used to evaluate control laws for flexible spacecraft—NASA/IEEE design challenge, Proc. of the Fourth VPI&SU Symposium on Dynamics and Control of Large Structures, (1984)
[6]
Robertson, Three-dimensional vibration analysis of a uniform beam with offset inertial masses at the ends, NASA Technical Memorandum 86393, (1985)
[7]
Yeo, Waldron, Goh, Optimal initial choice of multipliers in the quasilinearization method for optimal control problems with bounded controls, International Journal of Control, 20, pp. 17-33, (1974)
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Miele, Iyer, General technique for solving nonlinear two-point boundary-value problems via the method of particular solutions, J. Optim. Theory Applic., 5, pp. 382-399, (1970)
[9]
Li, Bainum, Minimum time attitude maneuvers of a rigid spacecraft, AIAA 26th Aerospace Sciences Meeting, (1988)
[10]
Li, Bainum, Numerical approach for solving rigid spacecraft minimum time attitude maneuvers, J. Guidance Control Dynam, 13, pp. 38-45, (1990)