Optimization of very-low-thrust, many-revolution spacecraft trajectories
Author:
Affiliation:
1. Spectrum Astro, Inc., Gilbert, Arizona 85233
2. University of Illinois, Urbana, Illinois 61801
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/10.2514/3.21331
Reference20 articles.
1. Discrete approximations to optimal trajectories using direct transcription and nonlinear programming
2. Optimal low-thrust transfers to synchronous orbit
3. Direct trajectory optimization using nonlinear programming and collocation
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