Solar-Sail Trajectory Design for a Multiple Near-Earth-Asteroid Rendezvous Mission
Author:
Affiliation:
1. University of Glasgow, Glasgow, Scotland G12 8QQ, United Kingdom
2. FH Aachen University of Applied Sciences, 52064 Aachen, Germany
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
http://arc.aiaa.org/doi/pdf/10.2514/1.G000470
Reference30 articles.
1. Multiple near-Earth asteroid rendezvous and sample return using first generation solar sailcraft
2. Generation of Optimal Trajectories for Earth Hybrid Pole Sitters
3. Dynamic and Structural Performances of a New Sailcraft Concept for Interplanetary Missions
4. Rapid design and optimization of low-thrust rendezvous/interception trajectory for asteroid deflection missions
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