Along-Track Boundedness Condition for Spacecraft Relative Motion Around a Slowly Rotating Asteroid
Along-Track Boundedness Condition for Spacecraft Relative Motion Around a Slowly Rotating Asteroid
复制标题
航天器绕慢速旋转小行星相对运动的沿轨有界条件
DOI:
10.1109/taes.2022.3183181
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发表时间:
2023-02
影响因子:
4.4
通讯作者:
Baoyin Hexi
中科院分区:
文献类型:
--
作者:
Wang Wei;Lei Hanlun;Mengali Giovanni;Quarta Aless;ro A;Baoyin Hexi
In this paper, the closed-form along-track boundedness condition for spacecraft relative motion around a slowly rotating asteroid is presented. As opposed to the previously proposed criteria where three necessary constraints must be satisfied, the current approach only requires to enforce one constraint to suppress the along-track drift, thus allowing two additional degrees of freedom in spacecraft formation design. In particular, to adapt the derived results applicable for formation with a relatively large size, the boundedness condition via first-order analysis is then extended to obtain a second-order result. In the latter case, the value of mean semimajor axis difference is found to be the root of a quadratic (algebraic) equation. Moreover, an optimal single-impulse maneuver is analyzed, by means of which the bounded relative motion can be guaranteed in the presence of initialization errors. Illustrative examples are provided to validate the analytical results.
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影响因子:
2.6
作者:
Changxuan Wen;P. Gurfil
通讯作者:
Changxuan Wen;P. Gurfil
DOI:
10.2514/1.g003837
发表时间:
2019-04
期刊:
Journal of Guidance, Control, and Dynamics
影响因子:
--
作者:
Lei Hanlun;Circi Christian;Ortore Emiliano;Condoleo Ennio;Xu Bo
通讯作者:
Xu Bo
影响因子:
5.6
作者:
Wang Wei;Mengali Giovanni;Quarta Aless;ro A;Yuan Jianping
通讯作者:
Yuan Jianping
DOI:
10.1016/j.asr.2012.06.001
发表时间:
2012-06
期刊:
ArXiv
影响因子:
--
作者:
M. Vasile;C. Maddock
通讯作者:
M. Vasile;C. Maddock
影响因子:
3.5
作者:
C. Circi;A. D’Ambrosio;Hanlun Lei;E. Ortore
通讯作者:
C. Circi;A. D’Ambrosio;Hanlun Lei;E. Ortore