Optimization of Variable-Specific-Impulse Gravity-Assist Trajectories
Author:
Affiliation:
1. Tsinghua University, 100084 Beijing, People’s Republic of China
Funder
National Natural Science Foundation of China
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Reference31 articles.
1. Low-Thrust Mission Design and Application
2. Development and Testing of the Hayabusa2 Ion Engine System
3. The physics and engineering of the VASIMR engine
4. Optimization of Variable-Specific-Impulse Interplanetary Trajectories
5. Optimal low-thrust transfer using variable bounded thrust
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2. A multi-objective variable-specific impulse maneuvers optimization methodology;Advances in Space Research;2024-01
3. On the Performance of Different Smoothing Methods for Indirect Low-Thrust Trajectory Optimization;The Journal of the Astronautical Sciences;2023-11-16
4. Generation of Multiple-Revolution Many-Impulse Optimal Spacecraft Maneuvers;Journal of Spacecraft and Rockets;2023-06-12
5. A Novel Variable Specific Impulse Optimization Methodology for Modulable Electric Propulsion Systems;AIAA SCITECH 2023 Forum;2023-01-19
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