本文關(guān)鍵詞：GEO航天器在軌燃料補給任務(wù)調(diào)度及優(yōu)化　出處：《南京航空航天大學(xué)》2016年碩士論文　論文類型：學(xué)位論文

  更多相關(guān)文章： 在軌燃料補給 空間燃料站 任務(wù)調(diào)度 遺傳算法

【摘要】：隨著航天技術(shù)的快速發(fā)展,航天活動的目標不僅是完成任務(wù),還要盡量延長航天器在軌壽命,同時深空探測的發(fā)展也受到燃料的限制,因此,在軌燃料補給技術(shù)越來越受到各航天大國的重視。此外,在軌燃料補給技術(shù)日益成熟,空間燃料站的設(shè)想也被提出,基于空間燃料站的在軌燃料補給任務(wù)調(diào)度研究具有很大的預(yù)研意義。本文以多個GEO航天器為在軌燃料補給對象,研究基于空間燃料站的在軌燃料補給的任務(wù)調(diào)度及優(yōu)化問題。首先,基于Battin方法求解多圈Lambert軌道轉(zhuǎn)移問題,得到了軌道轉(zhuǎn)移的速度增量和轉(zhuǎn)移時間的關(guān)系,加入末端滑行對兩者的關(guān)系進行優(yōu)化,便于將時間分配方案轉(zhuǎn)化為整數(shù)規(guī)劃問題;然后,研究了基于空間燃料站的在軌燃料補加任務(wù)模型,以GEO航天器為例,梳理在軌燃料補給任務(wù)中的變量和約束條件,以得到近似最優(yōu)服務(wù)順序和該順序下的近似最佳時間分配方案為優(yōu)化目標,構(gòu)建了GEO航天器在軌燃料補給任務(wù)調(diào)度模型;接著,基于遺傳算法,研究了GEO航天器在軌燃料補給任務(wù)調(diào)度算法;最后,在Matlab上對任務(wù)調(diào)度算法進行了數(shù)值仿真,仿真結(jié)果表明本文提出的方案是可行的。編寫界面化程序,形成了一個參數(shù)可設(shè)置的界面化的GEO航天器在軌燃料補給任務(wù)調(diào)度原型工具。
[Abstract]:With the rapid development of space technology, the goal of space activities is not only to complete the mission, but also to extend the on-orbit life of spacecraft as far as possible. At the same time, the development of deep space exploration is also limited by fuel. In addition, the on-orbit fuel recharge technology is becoming more and more mature, and the idea of space fuel station has also been put forward. The research of on-orbit fuel recharge task scheduling based on space fuel station is of great significance. In this paper, several GEO spacecraft are taken as in-orbit fuel recharge objects. The task scheduling and optimization problem of in-orbit fuel recharge based on space fuel station is studied. Firstly, the multi-cycle Lambert orbit transfer problem is solved based on Battin method. The relationship between the velocity increment and the transfer time of the orbit transfer is obtained, and the relationship between the two is optimized by adding the terminal glide, so that the time allocation scheme can be transformed into an integer programming problem. Then, the in-orbit fuel replenishment mission model based on space fuel station is studied. Taking the GEO spacecraft as an example, the variables and constraints in the in-orbit fuel replenishment mission are sorted out. Taking the approximate optimal service sequence and the approximate optimal time allocation scheme as the optimization objective, the on-orbit fuel supply task scheduling model of GEO spacecraft is constructed. Then, based on genetic algorithm, the scheduling algorithm of on-orbit fuel supply task for GEO spacecraft is studied. Finally, the task scheduling algorithm is numerically simulated on Matlab. The simulation results show that the proposed scheme is feasible. An interfacial GEO spacecraft on-orbit fuel replenishment task scheduling prototype tool with configurable parameters is developed.
【學(xué)位授予單位】：南京航空航天大學(xué)
【學(xué)位級別】：碩士
【學(xué)位授予年份】：2016
【分類號】：V52

【參考文獻】

相關(guān)期刊論文 前10條

1 梁彥剛;王偉林;;在軌服務(wù)航天器任務(wù)指派問題[J];國防科技大學(xué)學(xué)報;2013年05期

2 孔凡光;何建華;唐奎;;基于改進混合蛙跳算法的在軌服務(wù)飛行器任務(wù)分配[J];計算機測量與控制;2013年04期

3 郭筱曦;;歐洲自動轉(zhuǎn)移飛行器項目概覽[J];國際太空;2013年03期

4 丁建林;;基于兩行軌道參數(shù)的衛(wèi)星跟蹤應(yīng)用[J];中國科技信息;2012年08期

5 張琪新;孫富春;葉文;閔海波;;基于離散粒子群算法的航天器在軌服務(wù)任務(wù)分配問題研究[J];計算機測量與控制;2011年11期

6 任仙海;楊樂平;朱彥偉;;多GEO衛(wèi)星接近觀測任務(wù)規(guī)劃[J];飛行力學(xué);2011年03期

7 馮全勝;徐波;;基于伴飛模式的補給星軌道設(shè)計與優(yōu)化[J];宇航學(xué)報;2011年01期

8 歐陽琦;姚雯;陳小前;;地球同步軌道衛(wèi)星群在軌加注任務(wù)規(guī)劃[J];宇航學(xué)報;2010年12期

9 歐陽琦;趙勇;陳小前;;共面圓軌道航天器在軌服務(wù)任務(wù)規(guī)劃[J];中國空間科學(xué)技術(shù);2010年01期

10 梁斌;徐文福;李成;劉宇;;地球靜止軌道在軌服務(wù)技術(shù)研究現(xiàn)狀與發(fā)展趨勢[J];宇航學(xué)報;2010年01期

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