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Attitude Stability Analysis and Configuration Design of Pyramid Drag Sail for Deorbit Missions
Publisher: ASCE
Abstract: Deorbit disposal of constellation satellites at the end of their operational lifetime is considered a necessary task to maintain the safety and sustainability of low Earth orbit (LEO). In LEO region, especially below ...
Dynamics of Tethered-Coulomb Formation for Debris Deorbiting in Geosynchronous Orbit
Publisher: ASCE
Abstract: In order to reduce the population of space debris in geosynchronous orbit, a tethered-Coulomb formation (TCF) is proposed that consists of a space tug and a cluster of charged debris connected by elastic massless tethers. ...