New State Transition Matrix for Relative Motion on an Arbitrary Keplerian Orbit
New State Transition Matrix for Relative Motion on an Arbitrary Keplerian Orbit
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DOI:
10.2514/1.g002723
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发表时间:
2017-07
影响因子:
2.6
通讯作者:
Zhaohui Dang
中科院分区:
文献类型:
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作者:
Zhaohui Dang
A new formation of the relative state transition matrix has been developed for the spacecraft relative motion without using the Tschauner–Hempel solutions. The relative state transition matrix is o...