Analytical Guidance Solutions for Spacecraft Planar Rephasing via Input Shaping
Author:
Affiliation:
1. Department of Mechanical, Aerospace, and Nuclear Engineering, Rensselaer Polytechnic Institute, Troy, New York 12180
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.G000008
Reference18 articles.
1. Satellite formation flying using along-track thrust
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4. Vibration Reduction for Flexible Spacecraft Following Momentum Dumping With/Without Slewing
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