有限推力作用下航天器轨道优化设计方法分析

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1、-------哈尔滨工业大学工学硕士学位论文Accordingtorelativekineticstheory,somespecialformationswereanalyzedanddesignedfortheformationflyinginthecaseofcircularorbitandthenobtaininitialconditionsofcircleformationflying.Finally,applyingGausspseudospectralmethodgiveanexampleoforbitdesignforcircularformationflying.Keywor

2、dsFinitethrust;Trajectoryoptimization;Formationflying;GausspseudospectralmethodIII-----------哈尔滨工业大学工学硕士学位论文目录摘要.............................................................................................................................IAbstract.....................................................

3、..................................................................II第1章绪论................................................................................................................11.1课题背景和研究目的与意义...........................................................................11.2美国空间对抗系统发展情况.......

4、....................................................................21.2.1DART自主交会试验技术.........................................................................31.2.2NFIRE近地红外试验卫星........................................................................31.2.3试验卫星XSS系列..................................

5、................................................41.2.4TechSat21试验卫星系列...........................................................................41.3航天器轨道优化设计方法综述.......................................................................51.4本文主要研究内容.......................................................

6、....................................8第2章航天器轨道动力学模型................................................................................92.1引言...................................................................................................................92.2航天器轨道动力学模型..................................

7、.................................................92.2.1改进春分点根数形式的轨道动力学方程................................................9-----------2.2.1编队飞行相对动力学方程..........................................................