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RISOptimal Satellite-Formation Collision-Avoidance Maneuver Based on Relative E/I Vectors
Publisher: American Society of Civil Engineers
Multiobjective Optimization Design of TomoSAR Satellite Orbit Based on Multireference Transfer Orbit
Publisher: ASCE
Abstract: This paper investigates an optimal orbit design method for single-satellite synthetic aperture radar tomography (TomoSAR) missions. Satellites require multibaseline observations for three-dimensional imaging. Thus, we need ...