Orbit Design for Mars Exploration by the Accurate Dynamic Model

doi:10.3780/j.issn.1000-758X.2011.01.002

Abstract

Abstract: The precision orbit design for Mars exploration by the accurate dynamic model was studied. The launch window and trans-Mars orbit was determined through the partical swarm optimization (PSO) algorithm within the heliocentric two-body restriction. The patched conics method was introduced to design the earth-centred parking orbit and departure hyperbolic orbit. The solution of two-body Lambert problem was input as initial value for precision orbit design, and the preliminary orbit was corrected with the restrictions of the Mars B-plane parameters and flight time by the accurate dynamic model. Finally the designed orbit was simulated with the STK softwares.

Key words: Two-body problem, Differential iteration, Orbit design, Precision dynamic model, Mars probe, Simulation

CHEN Yang, ZHAO Guo-Qiang, BAOYin He-Xi, LI Jun-Feng. Orbit Design for Mars Exploration by the Accurate Dynamic Model[J]. Chinese Space Science and Technology, 2011, 31(1): 8-15.

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References

［1］KITZNER W. A method of describing miss distances for lunar and interplanetary trajectories[J]. Planetary and Space Science, 1961(7): 125-131. ［2］RAOFI B, BHAT R S, HELFRICH C. Propulsive maneuver design for the 2007 Mars phoenix lander mission[C]. AIAA/AAS Astrodynamics Specialist Conference and Exhibit, Honolulu, Hawaii, 2008. ［3］ROBIN M VAUGHAN, PIETER H KALLEMEYN JR, DAVID A. Spencer and Robert D. Braun. Navigation flight operations for mars pathfinder[J]. Journal of Spacecraft and Rockets, 1999, 36(3): 340-347. ［4］HOWARD D CURITS. Orbital mechanics for engineering students[M]. Elsevier Butterworth Heinemann, 2005. ［5］BATTIN R H. An introduction to the mathematics and methods of astrodynamics[M]. American Institute of Aeronautics and Astronautics, 1987. ［6］HOWARD D CURITS. Orbital mechanics for engineering students[M]. Elsevier Butterworth Heinemann, 2005. ［7］STEPHEN KEMBLE. Interplanetary mission analysis and design[M]. Berlin; New York, Springer; Chichester: Praxis Publishing, 2006. ［8］严辉, 吴宏鑫. 月球探测器轨道设计与地面观测弧[J]. 宇航学报, 1998, 19 (4): 70-74. YAN HUI, WU HONGXIN. Lunar trajectories and tracking arcs[J]. Journal of Astronautics, 1998, 19 (4): 70-74. ［9］谷立祥, 刘竹生. 使用遗传算法和B平面参数进行月球探测器转移轨道设计[J]. 导弹与航天运载技术, 2003, (3): 1-5.GU LIXIANG, LIU ZHUSHENG. Lunar trajectory design with GA and B-plane parameters[J]. Missiles and Space Vehicles, 2003 (3): 1-5. ［10］张晓文, 王大轶, 黄翔宇. 深空探测转移轨道自主中途修正方法研究[J]. 空间控制技术与应用, 2009, 35 (4): 27-33.ZHANG XIAOWEN, WANG DAYI, HUANG XIANGYU. Study on the autonomous midcourse correction during cruise phase of interplanetary exploration[J]. Aerospace Control and Application, 2009, 35 (4):27-33. ［11］张旭辉, 刘竹生. 火星探测器轨道设计与优化技术[J]. 导弹与航天运载技术, 2008(2): 15-23. ZHANG XUHUI, LIU ZHUSHENG. Trajectory design and optimization of mars satellite[J]. Missiles and Space Vehicles, 2008 (2): 15-23. ［12］高飞, 苏宪程. 火星探测器发射时机分析[J]. 装备技术指挥学院学报, 2009, 20 (4): 59-64.GAO FEI, SU XIANCHENG. Analysis of launch/arrival strategy for Mars probe[J]. Journal of the Academy of Equipment Command & Technology, 2009, 20 (4): 59-64. ［13］朱丽莉, 杨志鹏, 袁华. 粒子群优化算法分析及研究进展[J]. 计算机工程与应用, 2007, 43 (5): 24-27.ZHU LILI, YANG ZHIPENG, YUAN HUA. Analysis and development of particle swarm optimization[J]. Computer Engineering and Applications, 2007, 43 (5): 24-27. ［14］魏剑, 徐世杰. 火星探测器轨道运动建模的时空基准转换研究[J]. 中国空间科学技术, 2009, 29(2): 65-71. WEI JIAN, XU SHIJIE. Study of the timespace bench transformation of mars probe orbital motion modeling[J]. Chinese Space Science and Technology, 2009, 29(2): 65-71. ［15］JEFFREY S PARKER. The Bplane and its applications in interplanetary mission design[R]. Colorado: Jet Propulsion Laboratory, 2008.

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