Deorbiting spacecraft with passively stabilised attitude using a simplified quasi-rhombic-pyramid sail |
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Authors: | Narcís Miguel Camilla Colombo |
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Institution: | Department of Aerospace Science and Technology, Politecnico di Milano, Via la Masa, 34, 20156 Milan, Italy |
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Abstract: | This paper studies deorbiting using an analogue to the quasi-rhombic-pyramid concept for planar motion. The focus is on maintaining a stable (meaning oscillatory) attitude close to the direction of the velocity of the spacecraft relative to the atmosphere. The study consists of a massive computation of deorbit times chosen in a region of the phase space where atmospheric drag plays a leading role. Here, no damping effects are considered. Thus, any passive stabilisation observed is either due to solar radiation pressure or atmospheric drag. The results show that such stable deorbiting is feasible up to a threshold that depends upon the physical parameters of the sail. This threshold is around 500 km of altitude. Stable deorbiting is also shown to reduce the unpredictability that appears due to tumbling. |
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Keywords: | Solar sails End-of-life Solar radiation pressure Atmospheric drag Passive attitude stabilisation |
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