![9.6 星軌道轉(zhuǎn)移最省燃料仿真計(jì)算及結(jié)果分析](https://imgs.zsbeike.com/imgs/K/K09379/k09379.0133.5[0bb60260f48c].jpg)
 9.6.1仿真初值參數(shù)給出主衛(wèi)星的軌道要素初值:ac0=8000km,ec0=0.005,ic0=64.435deg,ωc0=90deg,Ωc0=0,Mc0=0(9.58)從衛(wèi)星軌道要素差的初值:在不考慮任何攝動(dòng)的情況下,主衛(wèi)星的軌道要素終值(tf自由):acf=8000km,ecf=0.005,icf=64.435deg,ωcf=90deg (共 956 字) [閱讀本文] >>
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 9.6.1仿真初值參數(shù)給出主衛(wèi)星的軌道要素初值:ac0=8000km,ec0=0.005,ic0=64.435deg,ωc0=90deg,Ωc0=0,Mc0=0(9.58)從衛(wèi)星軌道要素差的初值:在不考慮任何攝動(dòng)的情況下,主衛(wèi)星的軌道要素終值(tf自由):acf=8000km,ecf=0.005,icf=64.435deg,ωcf=90deg (共 956 字) [閱讀本文] >>