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| 书名 |
长寿卫星编队飞行理论基础 | | 并列正书名 |
Theoretical Basis of Long-term Satellite Formation Flight | | 丛书名 |
辽宁省优秀自然科学著作 | | 丛书多卷书否 |
Y | | ISBN |
978-7-5381-9287-2 | | 主要责任者 |
徐光延 | | 责任方式 |
著 | | 出版者 |
辽宁科学技术出版社 | | 出版地 |
沈阳 | | 出版日期 |
2015-07 | | 装帧 |
简 | | 页码 |
1-159 | | 字数 |
230 | | 定价 |
30.00 | | 作品语种 |
中 | | 整书中图分类号 |
V412.4 | | 参考文献 |
[1] Sabol C,Burns R,McLaughlin C A. Satellite Formation Flying Design and Evolution [J]. Journal of Spacecraft and Rockets,2001,38 (2): 270-278.
[2] Lane C,Axelrad P. Formation Design in Eccentric Orbits Using Linearized Equations of Relative Motion [J]. Journal of Guidance,Control,and Dynamics,2006,29 (1): 146-160.
[3] Scharf D P,Hadaegh F Y,Ploen S R. A Survey of Spacecraft Formation Flying Guidance and Control (Part Ⅰ): Guidance [C]. In Proceedings of the 2003 American Control Conference,2003,2: 1733-1739.
[4] Scharf D P,Hadaegh F Y,Ploen S R. A Survey of Spacecraft Formation Flying Guidance and Control (Part Ⅱ ): Control [C]. In Proceedings of the 2004 American Control Conference,2004,4: 2976-2985.
[5] Jiang F,Li J,Baoyin H,Gao Y. Study on Relative Orbit Geometry of Spacecraft Formations in Elliptical Reference Orbits [J]. Journal of Guidance,Control,and Dynamics,2008,31(1): 123-134.
[6] Sengupta P,Sharma R,Vadali S. Periodic Relative Motion near a Keplerian Elliptic Orbit with Nonlinear Differential Gravity [J]. Journal of Guidance,Control,and Dynamics,2006,29 (5): 1110-1121.
[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.
[8] Schaub H,Vadali S R,Junkins J L,Alfriend K T. Spacecraft Formation Flying Control Using Mean Orbit [J]. Journal of the Astronautical Sciences,2000,48 (1): 69-87.
[9] Sengupta P,Vadali S R,Alfriend K T. Averaged Relative Motion and Applications to Formation Flight near Perturbed Orbits [J]. Journal of Guidance,Control,and Dynamics,2008,31(2): 258-272.
[10] Vaddi S S,Alfriend K T,Vadali S R,Sengupta P. Formation Establishment and Reconfiguration Using Impulsive Control [J]. Journal of Guidance,Control,and Dynamics,2005,28 (2):262-268.
[11] Kechichian J A. Motion in General Elliptic Orbit with Respect to a Dragging and Precessing Coordinate Frame [J]. Journal of the Astronautical Sciences,1998,46 (1): 25-45.
[12] Xu G,Wang D. Nonlinear Dynamic Equations of Satellite Relative Motion around an Oblate Earth [J]. Journal of Guidance,Control,and Dynamics,2008,31 (5):1521-1524.
[13] Ross I M. Linearized Dynamic Equations for Spacecraft Subject to J2 Perturbations [J]. Journal of Guidance,Control,and Dynamics,2003,26 (4):657-659.
[14] Kasdin N,Gurfil P,Kolemen E. Canonical Modelling of Relative Spacecraft Motion via Epicyclic Orbital Elements [J]. Celestial Mechanics and Dynamical Astronomy,Springer,2005,92(4): 337-370.
[15] Schweighart S,Sedwick R. High-Fidelity Linearized J2 Model for Satellite Formation Flight[J]. Journal of Guidance,Control,and Dynamics,2002,25 (6): 1073-1080.
[16] Schweighart S,Sedwick R. Cross-Track Motion of Satellite Formation in Presence of J2 Disturbances [J]. Journal of Guidance,Control,and Dynamics,2005,28 (4):824-826.
[17] Xu G,Wang D. Dynamic Models of Satellite Relative Motion around an Oblate Earth [J]. Advances in the Astronautical Sciences,2008,130 (2): 1633-1648.
[18] Gim D W,Alfriend K T. State Transition Matrix of Relative Motion for the Perturbed Noncircular Reference Orbit [J]. Journal of Guidance,Control,and Dynamics,2003,26 (6):956-971.
[19] Alfriend K T,Yan H. Evaluation and Comparison of Relative Motion Theories [J]. Journal of Guidance,Control,and Dynamics,2005,28 (2): 254-261.
[20] Xu G,Wang D,Poh E K,Wu B. Periodic and Quasi-Periodic Satellite Relative Orbits at Critical Inclination [C]. 2009 IEEE Aerospace Conference,Big Sky,Montana,2009 (11):1911-1920.
[21] Hamel J,Lafontaine J. Linearized Dynamics of Formation Flying Spacecraft on a J2-Perturbed Elliptical Orbit [J]. Journal of Guidance,Control,and Dynamics,2007,30 (6):1649-1658.
[22] Schaub H. Relative Orbit Geometry through Classical Orbit Element Differences [J]. Journal of Guidance,Control,and Dynamics,2004,27 (5): 839-848.
[23] Sabatini M,Izzo D R,Bevilacqua R. Special Inclinations Allowing Minimal Drift Orbits for Formation Flying Satellites [J]. Journal of Guidance,Control,and Dynamics,2008,31 (1):94-100.
[24] Vadali S,Sengupta P,Yan H,Alfriend K T. Fundamental Frequencies of Satellite Relative Motion and Control of Formations [J]. Journal of Guidance,Control,and Dynamics,2008,31(5) : 1239-1248.
[25] Sabatini M,Izzo D R,Palmerini G B. Minimum Control for Spacecraft Formations in a J2 Perturbed Environment [C]. New Trends in Astrodynamics and Applications V,Milan,2008 (6):2123-2131.
[26] Wiesel W E. Relative Satellite Motion about an Oblate Planet [J]. Journal of Guidance,Control,and Dynamics,2002,25 (4): 776-785.
[27] Schaub H,Alfriend K T. J2 Invariant Reference Orbits for Spacecraft Formations [J]. Celestial Mechanics and Dynamical Astronomy,2001,79 (2): 77-95.
[28] Schaub H,Junkins J L. Analytical Mechanics of Space Systems [C]. American Institute of Aeronautics and Astronautics,Inc,Reston,VA,2003 (9): 1799-1820.
[29] Vadali S R,Alfriend K T,Vaddi S S. Hill＇s Equations Mean Orbital Elements and Formation Flying of Satellites [J]. Advances in the Astronautical Sciences,2000,106: 187-204.
[30] Eyer J K,Damaren C J. Quasi-Periodic Relative Trajectory Generation for Formation Flying Satellites [J]. Journal of Guidance,Control,and Dynamics,2009,32 (4): 1403-1406.
[31] Vignal P,Pernicka H. Low-Thrust Spacecraft Formation Keeping [J]. Journal of Spacecraft and Rockets,2006,43 (2): 466-475.
[32] Richards A,Schouwenaars T,How J P,Feron E. Spacecraft Trajectory Planning with Avoidance Constraints Using Mixed-Integer Linear Programming [J]. Journal of Guidance,Control,and Dynamics,2002,25 (4): 755-764.
[33] Redding D C,Adams N J. Linear-Quadratic Station Keeping for the STS Orbiter [J]. Journal of Guidance,Control,and Dynamics,1989,12 (2): 739-745.
[34] Zanon D J,Campbell M E. Optimal Planner for Spacecraft Formations in Elliptical Orbits[J]. Journal of Guidance,Control,and Dynamics,2006,29 (1): 161-171.
[35] Breger L,How J P. Gauss’s Variational Equation-Based Dynamics and Control for Formation Flying Spacecraft [J]. Journal of Guidance,Control,and Dynamics,2007,30 (2):437-448.
[36] Tillerson M,Inalhan G,How J P. Coordination and Control of Distributed Spacecraft Systems Using Convex Optimization Techniques [J]. International Journal of Robust and Nonlinear Control,2002,12 (2): 207-242.
[37] Gurfil P. Relative Motion between Elliptic Orbits: Generalized Boundedness Conditions and Optimal Formationkeeping [J]. Journal of Guidance,Control,and Dynamics,2005,28 (4):761-767.
[38] Wu B,Wang D,Poh E. K,Xu G. Nonlinear Optimization of Low-Thrust Trajectory for Satellite Formation: Legendre Pseudospectral Approach [J]. Journal of Guidance,Control,and Dynamics,2009,32 (4): 1371-1381.
[39] Gim D W,Alfriend K T. The State Transition Matrix of Relative Motion for the Perturbed NonCircular Reference Orbit [J]. Journal of Guidance,Navigation and Control,2003,26 (6):956-971.
[40] Arfken G. Mathematical methods for physicists [M]. 3rd ed. Orlando,FL: Academic Press,1985.
[41] Breger L,How J P. GVE-Based Dynamics and Control for Formation Flying Spacecraft[J]. Journal of Guidance,Control,and Dynamics,2007,30 (1):437-448.
[42] 曹喜滨,贺东雷. 编队构型保持模型预测控制方法研究 [J]. 宇航学报,2008,29 (4):1276-1283.
[43]吴宝林,曹喜滨.摄动椭圆参考轨道的相对运动状态转移方程 [J].宇航学报,2005,26 (1):702-706.
[44]李俊峰,孟鑫,高云峰,等. J2摄动对编队飞行卫星相对轨道构型的影响 [J].清华大学学报:自然科学版,2004,44 (2): 224-227.
[45] 孟鑫,李俊峰,高云峰.卫星编队飞行中相对轨道的J2摄动分析 [J].力学学报,2006,38(1): 89-96. | | 辞典简介 |
本册工具书是辽宁省优秀自然科学著作之一，共收录44条词条。 |
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