Collocation of Geostationary Satellites Using Convex Optimization
Author:
Affiliation:
1. DLR, German Aerospace Center, 28359 Bremen, Germany
2. Ben Gurion University of the Negev, 84105 Beer-Sheva, Israel
3. Delft University of Technology, 2629 HS Delft, The Netherlands
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.G001650
Reference15 articles.
1. Proximity Operations of Formation-Flying Spacecraft Using an Eccentricity/Inclination Vector Separation
2. Optimal Geostationary Satellite Collocation Using Relative Orbital Element Corrections
3. RauschR. R. “Relative Orbit Control or Collocated Geostationary Spacecraft,” Ph.D. Thesis, Purdue Univ., Lafayette, IN, 2012.
4. A Convex Guidance Algorithm for Formation Reconfiguration
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