Further improvements to a hybrid method for launch vehicle ascent trajectory optimization
- 14 August 2000
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 4 references indexed in Scilit:
- Design and Evaluation of a Three-Dimensional Optimal Ascent Guidance AlgorithmJournal of Guidance, Control, and Dynamics, 1998
- Direct trajectory optimization using nonlinear programming and collocationJournal of Guidance, Control, and Dynamics, 1987
- Optimal Analytic Multiburn TrajectoriesAIAA Journal, 1972
- Completely general closed-form solution for coordinates and partial derivative of the two-body problemThe Astronomical Journal, 1965