rendezvous problem 中文意思是什麼
rendezvous problem
解釋
集結問題, 聚集問題, 會合問題- rendezvous : n. 〈sing. , pl. 〉1. 【罕】指定集合地；集合基地；集合，結集。2. 約會，聚會，約會地點[時間]；幽會處。3. 太空船的會合（點）。vi. （尤指在約定地點）會合，會見，集合，聚會。
- problem : n. 1. 問題，課題；疑難問題；令人困惑的情況。2. 【數、物】習題；作圖題。3. （象棋的）布局問題。adj. 1. 成問題的；難處理的。2. 關于社會問題的。
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The basis of dynamics and simulation includes the iterative flyout angle algorithm to the solutions to lambert problem and battin ' s universal conic section state extrapolate method. then spacecraft ' s orbit roots, maneuver impulse and maneuver time are discussed as the following four part : first of all, the chaser ' s one orbit roots is selected as a variable to simulate its influence to the large scale orbital maneuver. the research reveals fact that the orbit roots both of chaser and target should be close to each other to achieve better maneuver and rendezvous " ability, moreover, the best orbit maneuver and rendezvous occurs when both chaser and target ' s initial phase angle are equal
為了研究了交會機動中追蹤器和目標器的軌道根數、機動時限和機動能耗等因素對交會機動的影響，模擬和分析分為以下四個部分:首先，研究了追蹤器軌道單個參數為變量情況下兩航天器大范圍交會機動問題，研究表明，追蹤器的變化參量與目標器相應的參量在接近的情況下可以獲得良好的交會機動特性，而對于兩航天器軌道共面的情況下，初始相位角相等時則獲得最佳的機動效果。 -
The dynamics model of rendezvous and docking, optimal rendezvous problem and the framework of the rendezvous and docking simulation system are studied in this thesis. the main achievements are summarized as following : 1
本文對交會對接模擬所需的動力學模型、空間交會的最優控制和交會對接模擬系統的總體框架進行了深入研究，並建立了交會對接模擬的原型系統。 -
Solution for optimal 3 - impulse rendezvous problem
三脈沖最優交會問題的解法
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