Warm Start for Low-Thrust Trajectory Optimization via Switched System
- 1 September 2021
- journal article
- research article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Guidance, Control, and Dynamics
- Vol. 44 (9), 1700-1706
- https://doi.org/10.2514/1.g005983
Abstract
No abstract availableFunding Information
- National Natural Science Foundation of China (11902174, 12022214)
This publication has 31 references indexed in Scilit:
- Time-optimal trajectories to circumsolar space using solar electric propulsionAdvances in Space Research, 2013
- Direct transcription of low-thrust trajectories with finite trajectory elementsActa Astronautica, 2012
- Practical Techniques for Low-Thrust Trajectory Optimization with Homotopic ApproachJournal of Guidance, Control, and Dynamics, 2012
- A Survey of Methods Available for the Numerical Optimization of Continuous Dynamic SystemsJournal of Optimization Theory and Applications, 2011
- Fuel-Optimal, Power-Limited Rendezvous with Variable Thruster EfficiencyJournal of Guidance, Control, and Dynamics, 2005
- Optimal control of switching systemsAutomatica, 2005
- Low Thrust Minimum-Fuel Orbital Transfer: A Homotopic ApproachJournal of Guidance, Control, and Dynamics, 2004
- Warm-Start Strategies in Interior-Point Methods for Linear ProgrammingSIAM Journal on Optimization, 2002
- Very low-thrust trajectory optimization using a direct SQP methodJournal of Computational and Applied Mathematics, 2000
- Survey of Numerical Methods for Trajectory OptimizationJournal of Guidance, Control, and Dynamics, 1998