Uncertainty Quantication and Control During Mars Powered Descent and Landing using Covariance Steering
Author:
Affiliation:
1. Georgia Institute of Technology
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2018-0611
Reference19 articles.
1. Guidance and Control System Design of the Viking Planetary Lander
2. Mars Pathfinder atmospheric entry - Trajectory design and dispersion analysis
3. Mars Exploration Entry, Descent and Landing Challenges
4. Entry, Descent, and Landing Performance of the Mars Phoenix Lander
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