Multiple Optima in Abort Ascent during Lunar Powered Descent
Author:
Affiliation:
1. San Diego State University
2. University of California San Diego
3. NASA Johnson Space Center
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2022-0949
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1. Optimal Abort Guidance and Experimental Verification Based on Feature Learning;Journal of Aerospace Engineering;2024-03
2. Opportunities for Team Development Based on Lessons Learned From Spaceflight Operations;2023 IEEE Aerospace Conference;2023-03-04
3. Feature-based Learning for Optimal Abort Guidance;AIAA SCITECH 2023 Forum;2023-01-19
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