New form for the optimal rendezvous equations near a Keplerian orbit
- 1 January 1990
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Guidance, Control, and Dynamics
- Vol. 13 (1) , 183-186
- https://doi.org/10.2514/3.20533
Abstract
No abstract availableKeywords
This publication has 9 references indexed in Scilit:
- Effects of propellant mass loss on fuel-optimal rendezvous near Keplerian orbitJournal of Guidance, Control, and Dynamics, 1989
- Fuel-optimal rendezvous near a point in general Keplerian orbitJournal of Guidance, Control, and Dynamics, 1987
- Fuel-optimal maneuvers of a spacecraft relative to a point in circular orbitJournal of Guidance, Control, and Dynamics, 1984
- Strategies and schemes for rendezvous on geostationary transfer orbitActa Astronautica, 1983
- Optimal impulsive transfer with time constraintActa Astronautica, 1982
- Optimal low-thrust rendezvous control.AIAA Journal, 1969
- Elliptic orbit rendezvous.AIAA Journal, 1967
- Second-order solution to the elliptical rendezvous problem.AIAA Journal, 1967
- ELLIPTIC ELEMENTS IN TERMS OF SMALL INCREMENTS OF POSITION AND VELOCITY COMPONENTSAIAA Journal, 1963