A State-Triggered Line of Sight Constraint for 6-DoF Powered Descent Guidance Problems
Author:
Affiliation:
1. University of Washington, Seattle
2. NASA Johnson Space Center
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2019-0924
Reference45 articles.
1. On the problem of optimal thrust programming for a lunar soft landing
2. OPTIMAL SPACE TRAJECTORIES
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