A closed-form solution for minimum-fuel, constant-thrust trajectories
- 1 July 1970
- journal article
- research article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 8 (7) , 1229-1234
- https://doi.org/10.2514/3.5877
Abstract
No abstract availableKeywords
This publication has 2 references indexed in Scilit:
- A Rapidly Convergent Descent Method for MinimizationThe Computer Journal, 1963
- The Optimization of TrajectoriesJournal of the Society for Industrial and Applied Mathematics, 1959