Computing the Set of Epsilon-Efficient Solutions in Multiobjective Space Mission Design
Author:
Affiliation:
1. CINVESTAV-IPN, San Pedro Zacatenco, 07360, Mexico
2. University of Strathclyde, Glasgow, G1 1XJ, United Kingdom
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Electrical and Electronic Engineering,Computer Science Applications,Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.46478
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1. Optimal multi-objective low-thrust spacecraft trajectories
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