Author:
Satak Neha,Davis Jeremy J.,Doebbler James,Hurtado John E.
Publisher
Springer Science and Business Media LLC
Subject
Space and Planetary Science,Aerospace Engineering
Reference12 articles.
1. GRUBIN, C. “Generalized Two-Impulse Scheme for Reorienting a Spin Stabilized Vehicle,” Progress in Astronautics and Rocketry, American Rocket Society, Guidance and Control, Vol. 8, New York, 1962, pp. 649 - 68.
2. PORCELLI, G. and CONNOLLY, A. “Optimal Attitude Control of a Spinning Space-Body - A Graphical Approach,” IEEE Transactions on Automatic Control, Vol. AC-12, No. 3, June 1967.
3. REDMOND, J. and SILVERBERG, L. “Fuel Optimal Reorientation of Axisymmetric Spin-Stabilized Satellites,” Journal of Guidance, Control, and Dynamics, Vol. 16, No. 1, pp. 217-219, 1993.
4. HALL, R. A. and KAZNACHEYEV, Y. V. “Fuel-Optimal Rotations of the Space Station Mir,” Proceedings of the AIAA, Guidance, Navigation and Control Conference, San Diego, CA, 29 -31 July 1996.
5. HALL, R. A., LOWRY, N. C., and GHORBEL, F. “Three-Pulse Minimal Fuel Rotations of Axisymmetric Spacecraft Using Reaction Control Thrusters,” Proceedings of the American Control Conference, Denver, Colorado June 4 - 6, 2003.