Minimum-fuel, power-limited transfers between coplanar elliptical orbits
- 1 January 1993
- journal article
- Published by Elsevier in Acta Astronautica
- Vol. 29 (1) , 1-15
- https://doi.org/10.1016/0094-5765(93)90064-4
Abstract
No abstract availableKeywords
This publication has 10 references indexed in Scilit:
- Optimal plane change during constant altitude hypersonic flightJournal of Guidance, Control, and Dynamics, 1991
- The solution of some difficult problems in low‐thrust interplanetary trajectory optimizationOptimal Control Applications and Methods, 1988
- Optimal low-thrust transfers to synchronous orbitJournal of Guidance, Control, and Dynamics, 1984
- Optimal low-thrust, limited power transfers between arbitrary elliptical orbitsActa Astronautica, 1977
- Analytical determination of the adjoint vector for optimum space trajectoriesJournal of Spacecraft and Rockets, 1970
- Canonical transformation applications to optimal trajectory analysis.AIAA Journal, 1969
- An asymptotic solution for optimum power limited orbit transfer.AIAA Journal, 1966
- Optimum power-limited orbit transfer in strong gravity fieldsAIAA Journal, 1965
- Errata: "Optimal Variable-Thrust Transfer of a Power-Limited Rocket between Neighboring Circular Orbits"AIAA Journal, 1964
- Optimum low-thrust rendezvous and station keepingAIAA Journal, 1964