Singular fuel-optimal space trajectories based on linearization about a point in circular orbit
- 1 September 1987
- journal article
- Published by Springer Nature in Journal of Optimization Theory and Applications
- Vol. 54 (3) , 447-470
- https://doi.org/10.1007/bf00940195
Abstract
No abstract availableKeywords
This publication has 12 references indexed in Scilit:
- Fuel-optimal maneuvers of a spacecraft relative to a point in circular orbitJournal of Guidance, Control, and Dynamics, 1984
- Minimum-fuel rocket trajectories involving intermediate-thrust arcsJournal of Optimization Theory and Applications, 1975
- Intermediate-thrust arcs and their optimality in a central, time-invariant force fieldJournal of Optimization Theory and Applications, 1973
- Optimal four-impulse fixed-time rendezvous in the vicinity of a circular orbit.AIAA Journal, 1969
- A survey of impulsive trajectories.AIAA Journal, 1969
- Optimal Space Trajectories—A Review of Published WorkThe Aeronautical Journal, 1968
- Necessary conditions for singular extremalsAIAA Journal, 1965
- Optimality of intermediate-thrust arcs of rocket trajectoriesAIAA Journal, 1965
- SINGULAR EXTREMALS IN LAWDEN'S PROBLEM OF OPTIMAL ROCKET FLIGHTAIAA Journal, 1963
- Terminal Guidance System for Satellite RendezvousJournal of the Aerospace Sciences, 1960