Trajectory Design Employing Convex Optimization for Landing on Irregularly Shaped Asteroids
Author:
Affiliation:
1. NASA Marshall Space Flight Center, Huntsville, Alabama 35812
2. San Diego State University, San Diego, California 92182
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Applied Mathematics,Electrical and Electronic Engineering,Space and Planetary Science,Aerospace Engineering,Control and Systems Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.G003045
Reference25 articles.
1. Implementation of the First Asteroid Landing
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4. A semi-analytical guidance algorithm for autonomous landing
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