Deorbiting Timing for Spacecraft in Geostationary Transfer Orbits Exploiting Luni–Solar Perturbations
Author:
Affiliation:
1. Beihang University, 100191 Beijing, People’s Republic of China
2. Technion—Israel Institute of Technology, 32000 Haifa, Israel
Funder
European Research Council Starting Independent Researcher Grant
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.A33938
Reference14 articles.
1. Combined Release and Radiation Effects Satellite (CRRES): Spacecraft and Mission
2. Single-event upset in geostationary transfer orbit during solar-activity maximum period measured by the Tsubasa satellite
3. Dynamical modeling and lifetime analysis of geostationary transfer orbits
4. The role of solar apsidal resonance in the evolution of geostationary transfer orbits
5. Dynamical properties of Geostationary Transfer Orbits over long time scales: consequences for mission analysis and lifetime estimation
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