Citation: | MENG Xin, LI Jun-feng, GAO Yun-feng. Useful Relative Motion Description Method for Perturbations Analysis in Satellite Formation Flying[J]. Applied Mathematics and Mechanics, 2005, 26(11): 1328-1336. |
[1] |
Clohessy W H,Wiltshire R S.Terminal guidance system for satellite rendezvous[J].Journal of the Aerospace Science,1960,27(5):653—658,674.
|
[2] |
Karlgaard C D,Lutze F H.Second-order relative motion equation[J].Journal of Guidance, Control, and Dynamics,2003,27(1):499—501.
|
[3] |
Schweighart S A,Sedwick R J.High-fidelity linearized J2 model for satellite formation flight[J].Journal of Guidance, Control, and Dynamics,2002,25(6):1073—1080. doi: 10.2514/2.4986
|
[4] |
Vaddi S S,Vadali S R,Alfriend K T.Formation flying: accommodating nonlinearity and eccentricity perturbations[J].Journal of Guidance, Control, and Dynamics,2003,26(2):214—223. doi: 10.2514/2.5054
|
[5] |
Sedwick R J, Miller D W,Kong E M C.Mitigation of differential perturbations in clusters of formation flying satellites[R]. AAS/AIAA Space Flight Mechanics Meeting, American Astronautical Society, AAS Paper,Feb,1999,99-124.
|
[6] |
Baoyin H,LI Jun-feng,GAO Yun-feng.Dynamical behaviors and relative trajectories of spacecrafts formation flying[J].Journal of Aerospace Science and Technology,2002,4(6):295—301.
|
[7] |
Inalhan G,Tillerson M,How J P.Relative dynamics and control of spacecraft formations in eccentric orbits[J].Journal of Guidance,Control, and Dynamics,2002,25(1):48—59. doi: 10.2514/2.4874
|
[8] |
Melton R G.Time explicit representation of relative motion between elliptical orbits[J].Journal of Guidance,Control, and Dynamics,2000,23(4):604—610. doi: 10.2514/2.4605
|
[9] |
李俊峰,高云峰,宝音贺西,等.卫星编队飞行动力学与控制研究[J].力学与实践,2002,24(2):1—6.
|
[10] |
高云峰,宝音贺西,李俊峰.卫星编队飞行动力学特性与相对轨道构形仿真[J].清华大学学报(自然科学版),2002,42(4):458—461.
|
[11] |
孟鑫,李俊峰,高云峰.编队飞行卫星相对运动的零J2摄动条件研究[J]. 清华大学学报(自然科学版),2004,44(2):219—223.
|
[12] |
LI Jun-feng,MENG Xin,GAO Yun-feng,et al.Study on relative orbital configuration in satellite formation flying[J].Acta Mechanica Sinica,2005,21(1):87—94. doi: 10.1007/s10409-004-0009-3
|
[13] |
章仁为.航天器轨道姿态动力学与控制[M].北京:北京航空航天大学出版社,1998.
|
[14] |
李俊峰,孟鑫,高云峰,等.J2摄动对编队飞行卫星相对轨道构形的影响[J].清华大学学报(自然科学版), 2004,44(2):224—227,251.
|
[1] | YU Xiao-jun. On Coordination Ratio of a Mixed Routing Game[J]. Applied Mathematics and Mechanics, 2013, 34(4): 420-426. doi: 10.3879/j.issn.1000-0887.2013.04.010 |
[2] | YUAN Chang-qing, LI Jun-feng, WANG Tian-shu, BAOYIN He-xi. Robust Attitude Control for Rapid Multi-Target Tracking in Spacecraft Formation Flying[J]. Applied Mathematics and Mechanics, 2008, 29(2): 169-180. |
[3] | ZHANG Zhi-guo, LI Jun-feng. Study on the Orbit and Attitude Control of Spacecraft Formation Flying[J]. Applied Mathematics and Mechanics, 2008, 29(1): 38-46. |
[4] | GONG Sheng-ping, LI Jun-feng, BAOYIN He-xi. Formation Around Planetary Displaced Orbit[J]. Applied Mathematics and Mechanics, 2007, 28(6): 675-683. |
[5] | GAO Yun-feng, BAOYIN He-xi, LI Jun-feng. Comparison of Two Methods in Satellite Formation Flying[J]. Applied Mathematics and Mechanics, 2003, 24(8): 799-804. |
[6] | WANG Jia-song, HE You-sheng. High-Resolution Numerical Model for Shallow Water Flows and Pollutant Diffusions[J]. Applied Mathematics and Mechanics, 2002, 23(7): 661-666. |
[7] | DAI Tian-min. New Principles of Power and Energy Rate of Incremental Rate Type for Generalized Continuum Field Theories[J]. Applied Mathematics and Mechanics, 2001, 22(12): 1243-1248. |
[8] | Fu Jingli, Chen Xiangwei, Luo Shaokai. Lie Symmetries and Conserved Quantities of Rotational Relativistic Systems[J]. Applied Mathematics and Mechanics, 2000, 21(5): 495-500. |
[9] | Luo Shaokai. The Theory of Relativistic Analytical Mechanics of the Rotational Systems[J]. Applied Mathematics and Mechanics, 1998, 19(1): 42-53. |
[10] | Zheng Wenhu. A Calculation Method to the Perturbation of a Satellite Caused by the Gravitation Field of the Earth[J]. Applied Mathematics and Mechanics, 1997, 18(2): 153-160. |
[11] | Hu Hurang, Wu Chengping. Analysis of Energy Release Rate for Cracked Laminates[J]. Applied Mathematics and Mechanics, 1995, 16(6): 527-541. |
[12] | Liang Fei, Zhang Shan-yuan. A Rate Type Method for Large Deformation Problems of Nonllnear Elasticity[J]. Applied Mathematics and Mechanics, 1994, 15(2): 121-128. |
[13] | Zhao Guo-qiao. Rated Generalized Sub-Region Variational Principles in Nonlinear Elastodynamics[J]. Applied Mathematics and Mechanics, 1993, 14(12): 1069-1075. |
[14] | Wang Cheng-wen. A Class of Kolmogorov’s Ecological System with Prey Having Constant Adding Rate[J]. Applied Mathematics and Mechanics, 1992, 13(4): 327-334. |
[15] | Guo Zhong-heng, Liang Hao-yun. Absolute Representations of Spins of Principal Frames in a Continuum[J]. Applied Mathematics and Mechanics, 1991, 12(1): 39-44. |
[16] | Gao Yang, E. T. Onat. Rate Variational Extremum Principles for Finite Elastoplasticity[J]. Applied Mathematics and Mechanics, 1990, 11(7): 617-624. |
[17] | Chen Yi-liang, Pope. S. B.. The Evolution Equation of Joint Pdf of Turbulent Velocity and Dissipation[J]. Applied Mathematics and Mechanics, 1989, 10(1): 23-32. |
[18] | Lü He-xiang, Tang Li-min, Liu Xiu-lan. The Curved Beam Element and Its Convergence Rate[J]. Applied Mathematics and Mechanics, 1989, 10(6): 487-498. |
[19] | Zhao De-wen, Zhang Qiang. Solution for Plane Strain Forward and Backward Extrusions with a Fractional Reduction R=0.5 by the Integration Depending on a Parameter[J]. Applied Mathematics and Mechanics, 1988, 9(4): 379-384. |
[20] | Guo Zhong-heng. Spin and Rotation Velocity of the Stretching Frame in Continuum[J]. Applied Mathematics and Mechanics, 1988, 9(12): 1045-1048. |