Optimal power-limited rendezvous with thrust saturation
Author:
Affiliation:
1. Worcester Polytechnic Institute, Worcester, Massachusetts 01609
2. Eastern Connecticut State University, Willimantic, Connecticut 06226
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/10.2514/3.21517
Reference38 articles.
1. Three-Dimensional Optimum Thrust Trajectories for Power Limited Propulsion Systems
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