Trajectory Design Employing Convex Optimization for Landing on Irregularly Shaped Asteroids
2016
23 pages
Report
Keine Angabe
Englisch
Astronautics , Spacecraft Trajectories & Flight Mechanics , Asteroids , Convexity , Design optimization , Descent trajectories , Gravitational fields , Trajectory optimization , Optimal control , Landing sites , Algorithms , Iterative solution , Nonlinearity , Planetary landing , Flight time , Propellant consumption
TRAJECTORY DESIGN EMPLOYING CONVEX OPTIMIZATION FOR LANDING ON IRREGULARLY SHAPED ASTEROIDS
British Library Conference Proceedings | 2016
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