Finite Horizon Optimal Nonlinear Spacecraft Attitude Control

Author:

Khamis Ahmed,Zydek Dawid

Publisher

Springer Science and Business Media LLC

Subject

Space and Planetary Science,Aerospace Engineering

Reference32 articles.

1. Sharma, R., Tewari, A.: Optimal nonlinear tracking of spacecraft attitude maneuvers. IEEE Trans Control Syst Technol 12(5), 677–682 (2004)

2. Cho, S., Cheng, Y.-M., Cochran, J.: Large angle maneuver of asymmetric spacecraft using solutions to the impulsive reorientation problem (aas 97–658). Adv. Astronaut. Sci. 97, 899–914 (1998)

3. Lin, Y., Kraige, L.: Enhanced techniques for solving the two-point boundary-value problem associated with the optimal attitude control of spacecraft. J. Astronaut. Sci. 37, 1–15 (1989)

4. Vadali, S., Junkins, J.: Optimal open-loop and stable feedback control of rigid spacecraft attitude maneuvers. J. Astronaut. Sci.(ISSN 0021-9142) 32, 105–122 (1984)

5. Banerjee, A.K.: Optimal feedback gains for three-dimensional large angle slewing of spacecraft. J. Guid. Control Dynam. 14(6), 1313–1315 (1991)

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