Impulsive Feedback Control to Establish Specific Mean Orbit Elements of Spacecraft Formations
Author:
Affiliation:
1. Sandia National Laboratories, Albuquerque, New Mexico 87185-1003
2. Texas A&M University, College Station, Texas 77843-3141
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/10.2514/2.4774
Reference12 articles.
1. Time-Explicit Representation of Relative Motion Between Elliptical Orbits
2. Spacecraft Formation Flying Control Using Mean Orbit Elements
3. Initial conditions and fuel-optimal control for formation flying of satellites
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