Optimization of low-thrust interplanetary trajectories using collocation and nonlinear programming
- 1 May 1995
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Guidance, Control, and Dynamics
- Vol. 18 (3) , 599-604
- https://doi.org/10.2514/3.21429
Abstract
No abstract availableKeywords
This publication has 9 references indexed in Scilit:
- Three-stage approach to optimal low-thrust Earth-moon trajectoriesJournal of Guidance, Control, and Dynamics, 1994
- Optimization of very-low-thrust, many-revolution spacecraft trajectoriesJournal of Guidance, Control, and Dynamics, 1994
- Discrete approximations to optimal trajectories using direct transcription and nonlinear programmingJournal of Guidance, Control, and Dynamics, 1992
- Optimal finite-thrust spacecraft trajectories using collocation and nonlinear programmingJournal of Guidance, Control, and Dynamics, 1991
- Direct trajectory optimization using nonlinear programming and collocationJournal of Guidance, Control, and Dynamics, 1987
- A collocation method for boundary value problemsNumerische Mathematik, 1972
- Approximate finite-thrust trajectory optimization.AIAA Journal, 1969
- Primer vector on fixed-time impulsive trajectories.AIAA Journal, 1968
- OPTIMUM INTERPLANETARY RENDEZVOUS WITH POWER-LIMITED VEHICLESAIAA Journal, 1963