Optimal power-limited rendezvous of a spacecraft with bounded thrust and general linear equations of motion

Author:

Carter T. E.

Publisher

Springer Science and Business Media LLC

Subject

Applied Mathematics,Management Science and Operations Research,Control and Optimization

Reference41 articles.

1. Space Technology;J. H. Irving,1959

2. Ross, S., andLeitmann, G.,Low Acceleration Trajectory Optimization in a Strong Central Force Field, Proceedings of the IAS Symposium on Vehicle Systems Optimization, New York, New York, pp. 127–131, 1961.

3. Edelbaum, T. N.,The Use of High and Low-Thrust Propulsion in Combination for Space Missions, Journal of the Astronautical Sciences, Vol. 9, pp. 49–60, 1961.

4. Saltzer, C., andFetheroff, C. W.,A Direct Variational Method for Calculation of Optimum Thrust Programs for Power-Limited Interplanetary Flight, Astronautica Acta, Vol. 7, pp. 8–20, 1961.

5. Melbourne, W. G.,Three-Dimensional Optimum Thrust Trajectories for Power-Limited Propulsion Systems, ARS Journal, Vol. 31, pp. 1723–1728, 1961.

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