The invention discloses a monopulse non-coplanar optimal near-moon capture method, which adopts a pure analytical method for calculation, does not need numerical integration, parameter optimization and search, can directly obtain an optimal orbital transfer point position and an orbital transfer speed increment vector direction and size, and is very suitable for on-board autonomous calculation. The method can be directly applied to programming of software on a future autonomous near-moon brake controller, and also has important reference value for autonomous fault diagnosis and disposal of near-moon brake.
本发明公开了一种单脉冲非共面最优近月捕获方法,该方法采用纯解析方法计算,无需数值积分,无需参数优化和搜索,可以直接获得最优变轨点位置和变轨速度增量矢量方向和大小,非常适合器上自主计算,可以直接应用于未来自主近月制动控制器上软件的编制,对近月制动的自主故障诊断与处置也有重要的参考价值。
Monopulse non-coplanar optimal near-moon capture method
一种单脉冲非共面最优近月捕获方法
2025-02-18
Patent
Electronic Resource
Chinese
IPC: | B64G Raumfahrt , COSMONAUTICS / G06Q Datenverarbeitungssysteme oder -verfahren, besonders angepasst an verwaltungstechnische, geschäftliche, finanzielle oder betriebswirtschaftliche Zwecke, sowie an geschäftsbezogene Überwachungs- oder Voraussagezwecke , DATA PROCESSING SYSTEMS OR METHODS, SPECIALLY ADAPTED FOR ADMINISTRATIVE, COMMERCIAL, FINANCIAL, MANAGERIAL, SUPERVISORY OR FORECASTING PURPOSES |
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