We present a framework for design-phase debris management for Walker-delta constellations that utilizes con-junction analysis between the proposed system and resident space objects. Our approach leverages optimization techniques focused on minimization or reduction of conjunction encounters and enables users to define key parameters to suit their needs. We also propose an optimization framework for active post-mission disposal, along with detailed analysis of the two different strategies based on high thrust and low thrust capabilities. Future extensions and applications of the constellation design process optimization and post-mission disposal optimization are discussed.
Optimization Framework for Minimal Conjunction Satellite Constellation Design and Post-Mission Disposal Trajectories
05.03.2022
5071623 byte
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
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