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- [2] ANALYTICAL GUIDANCE FOR SPACECRAFT RELATIVE MOTION UNDER CONSTANT THRUST USING RELATIVE ORBIT ELEMENTS SPACEFLIGHT MECHANICS 2013, PTS I-IV, 2013, 148 : 1979 - 1996
- [3] PERTURBATION EFFECTS ON ELLIPTICAL RELATIVE MOTION BASED ON RELATIVE ORBIT ELEMENTS SPACEFLIGHT MECHANICS 2012, 2012, 143 : 713 - +
- [4] STUDY OF ELLIPTICAL RELATIVE MOTION CONTROL BASED ON RELATIVE ORBIT ELEMENTS SPACEFLIGHT MECHANICS 2013, PTS I-IV, 2013, 148 : 3059 - 3076
- [5] SATELLITE RELATIVE MOTION IN ELLIPTICAL ORBIT USING RELATIVE ORBIT ELEMENTS ASTRODYNAMICS 2011, PTS I - IV, 2012, 142 : 1459 - 1478
- [6] Coupling analysis on relative motion of spacecraft attitude and orbit model based on dual quaternion Xibei Gongye Daxue Xuebao/Journal of Northwestern Polytechnical University, 2015, 33 (06): : 887 - 891
- [7] Nonlinear model of spacecraft relative motion in an elliptical orbit ADVANCES IN MECHANICS: THEORETICAL, COMPUTATIONAL AND INTERDISCIPLINARY ISSUES, 2016, : 177 - 181
- [8] DYNAMICS OF DEBRIS CLOUD MOTION BASED ON RELATIVE ORBIT ELEMENTS SPACEFLIGHT MECHANICS 2011, PTS I-III, 2011, 140 : 1011 - +
- [9] OSCULATING RELATIVE ORBIT ELEMENTS DESCRIBING RELATIVE SATELLITE MOTION ABOUT AN ECCENTRIC ORBIT ASTRODYNAMICS 2011, PTS I - IV, 2012, 142 : 1423 - 1439
- [10] Coupled attitude and orbit control for relative motion of underactuated spacecraft Kongzhi yu Juece/Control and Decision, 2014, 29 (06): : 969 - 978