A Comparison of Algorithms for Computing Differential Mean Orbital Elements in Formation Flying Missions
Author:
Affiliation:
1. Beihang University
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2013-4542
Reference21 articles.
1. The motion of a close earth satellite
2. Solution of the problem of artificial satellite theory without drag
3. Impulsive Feedback Control to Establish Specific Mean Orbit Elements of Spacecraft Formations
4. Formation Control of Satellites Subject to Drag Variations and J2 Perturbations
5. Gauss's Variational Equation-Based Dynamics and Control for Formation Flying Spacecraft
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