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An analytical approximation of ∆v for transfers in LEO is proposed, accounting for the effect of J2. Accuracy is verified by comparison to exact transfer optimization. The approximation can speed up the evaluation of large sequences of debris objects to be removed.
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This page is a summary of: Simple ΔV Approximation for Optimization of Debris-to-Debris Transfers, Journal of Spacecraft and Rockets, December 2020, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.a34831.
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