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作 者:Ping MA Weibo SUN Jie GAO Tao CHAO
机构地区:[1]Control and Simulation Center,Harbin Institute of Technology,Harbin 150001,China [2]Beijing Institute of Spacecraft System Engineering,Beijing 100094,China
出 处:《Chinese Journal of Aeronautics》2024年第9期385-398,共14页中国航空学报(英文版)
基 金:supported by the National Natural Science Foundation of China (No.62273119).
摘 要:To efficiently and accurately design satellite constellations equipped with Reentry Glide Vehicles(RGVs),new analytical solutions are developed for calculating their coverage perfor-mance.Specifically,a new coverage model is established by approximating the Reentry Reachable Domain(RRD).However,the computation of real-time relative distances between satellites and targets,which is essential for coverage analysis based on this model,imposes a significant compu-tational burden.To address this challenge,a coverage analysis method based on two-dimensional map theory is proposed.This method represents the coverage conditions of a target as a fixed area on a two-dimensional map and transforms the satellite trajectory into a series of parallel lines.By determining the intersection points between these lines and the area boundaries,the coverage ana-lytical solutions for a target point are derived.On this basis,coverage theorems are presented for rapid calculation of the constellation coverage performance for an area.Simulation results demon-strate the effectiveness and high precision of the proposed analytical solutions.
关 键 词:CONSTELLATION Analytical solutions Reentry glide vehicle Reentry reachable domain Two-dimensional map
分 类 号:V412.41[航空宇航科学与技术—航空宇航推进理论与工程]
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