Efficient ascent trajectory optimization using convex models based on the Newton–Kantorovich/Pseudospectral approach
- 1 July 2017
- journal article
- Published by Elsevier BV in Aerospace Science and Technology
- Vol. 66, 140-151
- https://doi.org/10.1016/j.ast.2017.02.023
Abstract
No abstract availableThis publication has 22 references indexed in Scilit:
- Reduced Transversality Conditions in Optimal Space TrajectoriesJournal of Guidance, Control, and Dynamics, 2013
- Newton–Kantorovich/Pseudospectral Solution to Perturbed Astrodynamic Two-Point Boundary-Value ProblemsJournal of Guidance, Control, and Dynamics, 2013
- Algorithm 902ACM Transactions on Mathematical Software, 2010
- Overview of some optimal control methods adapted to expendable and reusable launch vehicle trajectoriesAerospace Science and Technology, 2006
- Optimization of Launch Vehicle Ascent Trajectories with Path Constraints and Coast ArcsJournal of Guidance, Control, and Dynamics, 2001
- Design and Evaluation of a Three-Dimensional Optimal Ascent Guidance AlgorithmJournal of Guidance, Control, and Dynamics, 1998
- Survey of Numerical Methods for Trajectory OptimizationJournal of Guidance, Control, and Dynamics, 1998
- Energy management of three-dimensional minimum-time interceptJournal of Guidance, Control, and Dynamics, 1987
- Constrained Impulsive Trajectory Optimization for Orbit-to-Orbit TransferJournal of Guidance and Control, 1979
- DESIGN OF LUNAR AND INTERPLANETARY ASCENT TRAJECTORIESAIAA Journal, 1963