Solving Multi-objective Aeroassisted Spacecraft Trajectory Optimization Problems Using Extended NSGA-II
Author:
Affiliation:
1. Cranfield University
2. Beijing Institute of Technology
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2017-5193
Reference15 articles.
1. Fuzzy physical programming for Space Manoeuvre Vehicles trajectory optimization based on hp-adaptive pseudospectral method
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4. Interior-Point Approach to Trajectory Optimization
5. Entry Guidance Using Time-Scale Separation in Gliding Dynamics
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