Assessment of time spent in the LEO, GEO, and semi-synchronous zones by spacecraft on long-term reentering disposal orbits
Author:
Funder
US Department of the Air Force
Publisher
Elsevier BV
Subject
Aerospace Engineering
Reference16 articles.
1. “Orbital Lifetime and Collision Risk Reduction for Tundra Disposal Orbits,” Paper No. AAS 17-628;Jenkin,2017
2. Orbital lifetime and collision risk reduction for inclined geosynchronous disposal orbits;Jenkin;Acta Astronaut.,2019
3. Comparison of disposal options for Tundra orbits in terms of delta-V cost and long-term collision risk;Jenkin;J. Space Safe. Eng.,2021
4. Analysis of the long-term dynamical evolution of the inclined geosynchronous orbits in the Chinese BeiDou navigation system;Zhao;Adv. Space Res.,2015
5. Long-term evolution of the inclined geosynchronous orbit in BeiDou navigation satellite system;Tang;Adv. Space Res.,2017
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3. Analysis of Near-Earth Space for the Search of Optimal Orbits for Placement of Satellites;Russian Physics Journal;2024-07
4. Uncertainty-aware Cube algorithm for medium-term collision risk assessment;Advances in Space Research;2023-01
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