Robust Guidance and Control Algorithms Using Constant Flight Path Angle for Precision Landing on Mars
Author:
Affiliation:
1. NGC Aerospace Ltd.
2. Université de Sherbrooke
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2006-6075
Reference25 articles.
1. Mars Pathfinder atmospheric entry - Trajectory design and dispersion analysis
2. Trajectory control for a low-lift re-entry vehicle
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