共 50 条
- [22] ELECTROSTATICALLY CHARGED SPACECRAFT FORMATION ESTIMATION USING LINEARIZED RELATIVE ORBIT ELEMENTS SPACEFLIGHT MECHANICS 2017, PTS I - IV, 2017, 160 : 3503 - 3519
- [23] Some Integrals Observed in Spacecraft Relative Motion Problem with Circular Reference Orbit 2016 IEEE CHINESE GUIDANCE, NAVIGATION AND CONTROL CONFERENCE (CGNCC), 2016, : 2450 - 2455
- [25] NONLINEAR REDUCED ORDER DYNAMICS OF SPACECRAFT RELATIVE MOTION FOR A CIRCULAR CHIEF ORBIT ASTRODYNAMICS 2015, 2016, 156 : 3505 - 3524
- [27] Some integrals observed in spacecraft relative motion problem with circular reference orbit CGNCC - IEEE Chin. Guid., Navig. Control Conf., 1600, (2450-2455):
- [28] Canonical modelling of relative spacecraft motion via epicyclic orbital elements CELESTIAL MECHANICS & DYNAMICAL ASTRONOMY, 2005, 92 (04): : 337 - 370
- [29] DECOMPOSITION ANALYSIS OF SPACECRAFT RELATIVE MOTION UNDER PERTURBATIONS FOURTH IAA CONFERENCE ON DYNAMICS AND CONTROL OF SPACE SYSTEMS 2018, PTS I-III, 2018, 165 : 1955 - 1971
- [30] Canonical Modelling of Relative Spacecraft Motion Via Epicyclic Orbital Elements Celestial Mechanics and Dynamical Astronomy, 2005, 92 : 337 - 370