Descent & Landing Trajectory and Guidance Algorithms with Divert Capabilities for Moon Landing
Author:
Affiliation:
1. European Space Agency
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2024-0086
Reference34 articles.
1. Using Virtual Reality to Design and Evaluate a Lunar Lander: The EL3 Case Study
2. Klumpp, A. R. "Apollo Lunar-Descent Guidance," Tech. Rep. R-695, MIT Charles Stark Draper Laboratory, 1971.
3. Survey of Numerical Methods for Trajectory Optimization
4. On the implementation of an interior-point filter line-search algorithm for large-scale nonlinear programming
5. Convex Optimization for Trajectory Generation: A Tutorial on Generating Dynamically Feasible Trajectories Reliably and Efficiently
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