卫星星座构形控制与设计研究
|
摘要
星座构形设计是星座部署和运行的前提。星座部署和运行的性能要求是影响星座构形设计的重要性能指标。论文针对星座构形与运行维持性能要求的相互影响,分别对卫星星座的摄动补偿策略、构形控制、空间备份策略、以及区域导航星座和分阶段部署导航星座的优化设计等问题进行了研究。
通过分析卫星星座的基本轨道以及星座构形基本约束,建立了星座基本构形和状态描述模型。研究了星座几何构形与运行维持性能的关系,包括星座构形的最大容许漂移量、长期稳定性、性能台阶、容错性以及可扩展性等。
通过分析卫星轨道、星座构形和星座性能的稳定性,设计了星座构形优化设计的参数偏置摄动补偿策略,通过摄动补偿的方法对星座构形参数进行优化设计,提高了星座构形稳定性,并且分析了摄动补偿策略的适应条件和范围。
分析了星座构形控制的特点和过程,明确了星座构形控制任务。基于覆盖性能要求进行了星座构形最大容许漂移量的计算。提出了分段离散序列控制策略并将其应用于星座构形设计。针对星座故障或失效卫星的存在问题,提出了相邻相位和均匀相位的星座构形沿航迹重构控制策略,建立了考虑燃料消耗、重构时间、燃料消耗均匀性、性能修复程度综合最优的星座构形变换优化准则,实现星座构形沿航迹失效重构。以天基多基地雷达星座为背景,进行了区域覆盖星座构形和控制策略优化设计研究。
从提高备份卫星可用性的角度进行备份轨道的选择和设计,建立了星座空间备份策略设计性能模型,提出了基于卫星可靠度和平均修复时间的星座空间备份策略优化设计方法。
基于区域导航星座的GEO/IGSO/MEO基本结构,考虑区域导航星座设计的基本需求和约束,建立了星座设计优化数学模型,基于多岛遗传算法优化策略进行多目标多约束条件下区域导航星座全局优化设计,得到了多个满足任务需求的设计方案。针对区域导航星座扩展性能要求进行了基于基准构型的区域导航星座扩充优化设计。结合区域导航星座任务特点,基于摄动补偿策略对星座构形进行了优化设计,提高了星座构形稳定性。
分析了导航星座部署的阶段性特点,设计了分阶段部署导航星座基本结构,明确了分阶段部署导航星座设计目标和与约束,建立了分阶段部署导航星座优化设计模型,综合考虑星座构形长期稳定性、构形控制、系统可靠性、系统费用、部署策略、备份策略等性能约束并结合我国导航星座实际任务需求,基于多目标进化算法的优化策略和线性加权和法的多目标决策进行了分阶段部署导航星座的多目标优化设计。
The constellation design is the premise of the deployment and the operation of satellite constellation, and the performance requirements on the deployment and the operation of satellite constellation are the important factors that affect the constellation design. Considering the constraint relations between the configuration and the operation of satellite constellation, the optimization design problems are studied on the perturbation compentation strategy, the configuration control, the spatial backup strategy, the regional coverage navigation constellation and the staged deployment navigation constellation.
The basic orbits of satellite constellation and the basic restraints of constellation configuration are analyzed, and the basic configuration models and the state description models for satellite constellation are established. The relationships between the constellation geometry configuration and the performance of the operation and maintenance are studied, which include the allowable drifting most greatly, the long-term stability, the performance stair, the fault tolerance as well as the extendibility demand for constellation configuration.
The stability of the satellite orbit, the constellation configuration and performance is analyzed. Based on the active deviation of the orbital parameters, the compentation strategy on the perturbation is designed, then the configuration optimaztion for the constellation using the compenstation strategy is finished, and the configuration stability of the satellite constellation is improved, and its suitable conditions and scopes also are analyzed.
The characteristics and the process of the constellation configuration control are analyzed, and the control missions of the satellite constellation are determined. Based on the coverage performance requirements, the allowable drifting most greatly of the constellation configuration is computed. The partition separate sequence control strategy is presented, and applies it in the design of the constellation configuration. In view of the problems about the satellite breakdown or the satellite expiration, the reconfiguration control strategies including the neighboring phase and the even phase of the constellation configuration along-track are presented. The most superior constellation configuration transformation optimization criterions are established that the criterions considered the fuel consumption, the reconfiguration time, the fuel consumption uniformity and the performance repaired and all so, and the constellation configuration along-track expiration reconfiguration is realized. Take the space borne multistatic radar constellation as the background, the studies has carried on the regional coverage constellation configuration optimization design and the coordination control strategy.
From the view to enhance the availability of the backup satellite, the orbit of the backup satellite is choice and designed, and the design performance analysis models of the constellation spatial backup strategy are established, and then the constellation spatial backup strategy optimization design method is presented based on the satellite reliability and MTTR (Mean Time To Repair).
Based on the basic structures of the regional navigation constellation, the basic requirements and constraints of the regional navigation constellation are considered, and the mathematical model of the constellation optimization design is established. Based on the optimization strategy of MIGA (Multi-Island Genetic Algorithm), the global optimization design of the regional navigation constellation under the multi-objectives and the multi-constraints is carried on, and some design results, which meet mission requirements, are obtained. In view of the expansion performance requirements of the regional navigation constellation, the expansion optimization design of the regional navigation constellation based on the basic configuration is carried on. Considering the mission characteristics of the regional navigation constellation, the configuration design for the regional navigation constellation based on the compenstation strategy for the perturbations is finished.
The staged characteristics of the deployment of the navigation constellation are analyzed, and the basic structure of the staged deployment navigation constellation is designed, and the design objectives and constraints of the staged deployment navigation constellation are determined, and then the optimization design models of the staged deployment navigation constellation are established. Overall considering the performance constraints including the configuration long-term stability, the configuration control, the system reliability, the system expense, the deployment strategy and the spatial backup strategy and so on and the mission requirements of the navigation constellation for our country, and then it is carried on the multi-objective optimization design of the staged deployment navigation constellation based on the optimization strategy of the multi-objective evolution algorithm and the multi-objective decision making of the linear weighted sum method.
通过分析卫星星座的基本轨道以及星座构形基本约束,建立了星座基本构形和状态描述模型。研究了星座几何构形与运行维持性能的关系,包括星座构形的最大容许漂移量、长期稳定性、性能台阶、容错性以及可扩展性等。
通过分析卫星轨道、星座构形和星座性能的稳定性,设计了星座构形优化设计的参数偏置摄动补偿策略,通过摄动补偿的方法对星座构形参数进行优化设计,提高了星座构形稳定性,并且分析了摄动补偿策略的适应条件和范围。
分析了星座构形控制的特点和过程,明确了星座构形控制任务。基于覆盖性能要求进行了星座构形最大容许漂移量的计算。提出了分段离散序列控制策略并将其应用于星座构形设计。针对星座故障或失效卫星的存在问题,提出了相邻相位和均匀相位的星座构形沿航迹重构控制策略,建立了考虑燃料消耗、重构时间、燃料消耗均匀性、性能修复程度综合最优的星座构形变换优化准则,实现星座构形沿航迹失效重构。以天基多基地雷达星座为背景,进行了区域覆盖星座构形和控制策略优化设计研究。
从提高备份卫星可用性的角度进行备份轨道的选择和设计,建立了星座空间备份策略设计性能模型,提出了基于卫星可靠度和平均修复时间的星座空间备份策略优化设计方法。
基于区域导航星座的GEO/IGSO/MEO基本结构,考虑区域导航星座设计的基本需求和约束,建立了星座设计优化数学模型,基于多岛遗传算法优化策略进行多目标多约束条件下区域导航星座全局优化设计,得到了多个满足任务需求的设计方案。针对区域导航星座扩展性能要求进行了基于基准构型的区域导航星座扩充优化设计。结合区域导航星座任务特点,基于摄动补偿策略对星座构形进行了优化设计,提高了星座构形稳定性。
分析了导航星座部署的阶段性特点,设计了分阶段部署导航星座基本结构,明确了分阶段部署导航星座设计目标和与约束,建立了分阶段部署导航星座优化设计模型,综合考虑星座构形长期稳定性、构形控制、系统可靠性、系统费用、部署策略、备份策略等性能约束并结合我国导航星座实际任务需求,基于多目标进化算法的优化策略和线性加权和法的多目标决策进行了分阶段部署导航星座的多目标优化设计。
The constellation design is the premise of the deployment and the operation of satellite constellation, and the performance requirements on the deployment and the operation of satellite constellation are the important factors that affect the constellation design. Considering the constraint relations between the configuration and the operation of satellite constellation, the optimization design problems are studied on the perturbation compentation strategy, the configuration control, the spatial backup strategy, the regional coverage navigation constellation and the staged deployment navigation constellation.
The basic orbits of satellite constellation and the basic restraints of constellation configuration are analyzed, and the basic configuration models and the state description models for satellite constellation are established. The relationships between the constellation geometry configuration and the performance of the operation and maintenance are studied, which include the allowable drifting most greatly, the long-term stability, the performance stair, the fault tolerance as well as the extendibility demand for constellation configuration.
The stability of the satellite orbit, the constellation configuration and performance is analyzed. Based on the active deviation of the orbital parameters, the compentation strategy on the perturbation is designed, then the configuration optimaztion for the constellation using the compenstation strategy is finished, and the configuration stability of the satellite constellation is improved, and its suitable conditions and scopes also are analyzed.
The characteristics and the process of the constellation configuration control are analyzed, and the control missions of the satellite constellation are determined. Based on the coverage performance requirements, the allowable drifting most greatly of the constellation configuration is computed. The partition separate sequence control strategy is presented, and applies it in the design of the constellation configuration. In view of the problems about the satellite breakdown or the satellite expiration, the reconfiguration control strategies including the neighboring phase and the even phase of the constellation configuration along-track are presented. The most superior constellation configuration transformation optimization criterions are established that the criterions considered the fuel consumption, the reconfiguration time, the fuel consumption uniformity and the performance repaired and all so, and the constellation configuration along-track expiration reconfiguration is realized. Take the space borne multistatic radar constellation as the background, the studies has carried on the regional coverage constellation configuration optimization design and the coordination control strategy.
From the view to enhance the availability of the backup satellite, the orbit of the backup satellite is choice and designed, and the design performance analysis models of the constellation spatial backup strategy are established, and then the constellation spatial backup strategy optimization design method is presented based on the satellite reliability and MTTR (Mean Time To Repair).
Based on the basic structures of the regional navigation constellation, the basic requirements and constraints of the regional navigation constellation are considered, and the mathematical model of the constellation optimization design is established. Based on the optimization strategy of MIGA (Multi-Island Genetic Algorithm), the global optimization design of the regional navigation constellation under the multi-objectives and the multi-constraints is carried on, and some design results, which meet mission requirements, are obtained. In view of the expansion performance requirements of the regional navigation constellation, the expansion optimization design of the regional navigation constellation based on the basic configuration is carried on. Considering the mission characteristics of the regional navigation constellation, the configuration design for the regional navigation constellation based on the compenstation strategy for the perturbations is finished.
The staged characteristics of the deployment of the navigation constellation are analyzed, and the basic structure of the staged deployment navigation constellation is designed, and the design objectives and constraints of the staged deployment navigation constellation are determined, and then the optimization design models of the staged deployment navigation constellation are established. Overall considering the performance constraints including the configuration long-term stability, the configuration control, the system reliability, the system expense, the deployment strategy and the spatial backup strategy and so on and the mission requirements of the navigation constellation for our country, and then it is carried on the multi-objective optimization design of the staged deployment navigation constellation based on the optimization strategy of the multi-objective evolution algorithm and the multi-objective decision making of the linear weighted sum method.
引文
[1]白鹤峰.卫星星座的分析设计与控制方法研究[D].国防科技大学研究生院工学博士学位论文.1999.4.
[2]Thunnissen DP,Balancing Cost,Risk,and Performance Under Uncertainty in Preliminary Mission Design[A].AIAA 2004-5878,Space 2004 Conference and Exhibit[C],San Diego,CA,28-30 Sept.2004.
[3]Kelley CW.Minimizing the cost of availability of services from a constellation of satellites[D].Ph.D Thesis,University of Southern California,Los Angles,CA,2003.
[4]项军华,张育林.卫星星座的自主位置保持[A].全国第十一届空间及运动体控制技术学术会议[C],云南昆明,2004.8,215-220.
[5]Martin Peiro AB,Beech TW,Alvaro Mozo Garcia et al.Galileo In-Orbit Control Strategy[A].Proceedings of the IAIN World Congress in association with the U.S.ION Annual Meeting[C],26-28,Jun.,2000,San Diego,CA.,469-480.
[6]Wertz JR,Gwynne Gurevich.Applications of Autonomous On-Board Orbit Control[A],11th AAS/AIAA Space Flight Mechanics Meeting[C],Santa Barbara,CA,11 - 15 Feb.2001.
[7]Walt Truszkowsk,David Zoch,Dan Smith.Autonomy for Constellations[Z].http://agents.gsfc.nasa.gov/papers/index.html.
[8]Ananda MP,Bernstein H,Cunningham KE et al.,Global Position System(GPS)Autonomous Navigation[J].Inst.of Electrical and Electronics Engineer Position Location and Navigation Symposium,Inst.of Electrical and Electronics Engineers,New York,1990.
[9]Swan PA.A Revolution in Progress:IRIDIUM LEO Operations.AIAA-97-3954.AIAA Defense and Space Programs Conference and Exhibit - Critical Defense and Space Programs for the Future,Huntsville,AL;UNITED STATES;23-25 Sept.1997.158-163.1997.
[10]John Tandler.Automating the Operations of the ORBCOMM Constellation[A].10th Annual AIAA/Utah State University Conference on Small Satellites[C],North Logan,UT.Sept.1996.
[11]Andrew W.Lewin.Low-Cost Operation of the ORBCOMM Satellite Constellation[J].Journal of Reducing Space Mission Cost.Mar.1998.1(1):105-117.
[12]Clifford W.Kelley,Transition to a 30 Satellite GPS Constellation[A].Proceedings ION NTM 1998[C],Jan.1998.371-380.
[13]Clifford W.Kelley,Steven C.Fisher.Orbital Optimization of the GPS Constellation and Its Effect on Accuracy and Availability[A].Proceeding of ION GPS-97[C],Sept.16-19,1997,Kansas City,MO.423-435.
[14]Turner AE,Rodden JJ,Melvin T et al.,GlobalStarTM Constellation Design and Establishment Experience[A].AAS/AIAA Astrodynamics Conference Advances in the Astronautical Sciences[C],MT,US,August 3-7,2003.116(3):2127-2143.
[15]范丽.卫星星座一体化优化设计研究[D].国防科技大学博士学位论文,2006.3.
[16]Olivier De Wech,Richard de Neufville,Mathieu Chaize et al.,Enhancing the Economics of Satellite Constellation via Staged Deployment[P].International Telecommunications Union Strategy and Policy Unit,Geneva,1 July 2004.
[17]Lefebvre L,Lamy A,Brousse P et al.Relative Station Keeping Optimization for the Starsys Constellation[A],Proceedings of the 12th International Symposium on Space Flight Dynamics[C],ESOC,Darmstadt.Germany.2-6 Jun.1997.
[18]张洪华,李鸿铭,邹广瑞,李昕.圆轨道星座位置保持控制的仿真与研究[J].中国空间科学技术,(6):15-23.2000.12.
[19]张晓敏.航天器相对轨道动力学与控制研究[D].北京航空航天大学博士学位论文,2000.
[20]Dong-Woo Gim,Kyle T.Alfriend.The State Transition Matrix of Relative Motion for the Perturbed Non-circular Reference Orbit[A].AAS 01-222,AAS/AIAA Space Flight Mechanics Meeting[C],11-15 Feb.2001,San Diego,CA.1-23.
[21]Chao CC,Bowen AF.Effects of Long-term Orbit Perturbations and Injection errors on GPS Constellation Values[A].AIAA 86-2173,Astrodynamics Conference[C],August 18-20,1986,Williamsburg,VA.
[22]胡松杰,陈力,刘林.卫星星座的结构演化[J].天文学报,Feb.,2003,44(1):46-54.
[23]Deleflie F,Legendre P,Exertier P et al.,Long Term Evolution of the Galileo Constellation due to Gravitation Forces[J].Advances in Space Research,2005,36:402-411.
[24]Marek Ziebart,Sima Adhya.GPS Block ⅡR Non-Conservative Force Modelling:Computation and Implications[A].ION GPS/GNSS 2003[C],Portland,OR.9-12 Sept.2003.2671-2678.
[25]Marek Ziebart,Sima Adhya,Ant Sibthorpe et al.Taking the Long View:The Impact of Spacecraft Structural Design and Hign Precision Force Modeling on Long-term Orbit Evolution[A].ION GPS/GNSS 2003[C],Portland,OR.9-12 Sept.2003,1002-1008.
[26]Chao CC.Long-Term Orbit Perturbation of the Draim Four-Satellite Constellation[J].AIAA 90-2900,AIAA/AAS Astrodynamics Conference,Portland,OR,Aug 20-22,1990.Technical Papers.Pt.1(A90-52957 24-13).Washington,DC,American Institute of Aeronautics and Astronautics,1990.208-213.
[27]Schutz BE,Craig DE.GPS Orbit Evolution:1998-2000[A].AIAA 2000-4237,AIAA/AAS Astrodynamics Specialist Conference[C],Denver,CO.14-17,Aug.2000.
[28]Lamy A,Pascal S.Station Keeping Strategies for Constellations of Satellites[J],Spaceflight Dynamics,1993.84:819-833.
[29]Brodsky P,Chen S M-S.Automatic Maneuver Planning for Maintenance of Satellite Constellation Geometry[A]In:Flight Mechanics Symposium 1997[C],Greenbelt,MD,19-21 May 1997.397-404.
[30]Glickman RE.TIDE:The Timed-Destination Approach to Constellation Formationkeeping,[A]AAS 94-122,In:Spaceflight Mechanics 1994;Proceedings of the 4th AAS/AIAA Spaceflight Mechanics Meeting[C],Cocoa Beach,FL,14-16 Feb.,1994.
[31]Ulybyshev U.Long-Term Formation Keeping of Satellite Constellation Using Linear-Quadratic Controller[J].Journal of Guidance,Control,and Dynamics,1998,21(1),109-115.
[32]Lasserre E,Dufour F,Bernussou et al.A Linear Programming Solution to the Homogeneous Satellite Constellation StationKeeping[A].IA9-97-A.4.08,48th International Astronautical Congress[C],Turin,Italy,6-10 Oct.,1997.
[33]McInnes CR.Autonomous Ring Formation for a Planar Constellation of Satellites[J].Journal of Guidance,Control,and Dynamics,Oct.1995,18(5):1215-1217.
[34]Evandro Marconi Rocco Marcelo,Lopes de Oliveira e Souza Antonio,Fernando Bertachini de Almeida Prado.Multi-Objective Optimization Approach Applied to StationKeeping of Satellite Constellations[A],AAS/AIAA Astrodynamics Conference[C],Jul.30-Aug.2,2001,Quebec City,Quebec,Canada.
[35]向开恒,卫星星座站位保持与控制研究[D],北京航空航天大学博士学位论文,1999.
[36]Randal Beard.Architecture and Algorithms for Constellation Control[R].Final Report,Brigham Young University,16 Mar.1998.
[37]Jean-Louis Calvet,Ghita Kardoudi.A Multilevel Approach for the Station-keeping of a Phased Satellite Constellation[A],13th Triennial World Congress[C],San Francisco,USA.
[38]Rondinelli G,Cramarossa A,Graziani F.Orbit Control Strategy for a Constellation of Three Satellites in Tundra Orbits[A].AAS 89-411,AAS/AIAA Astrodynamics Specialist Conference[C],7-10 Aug.1989.1-13.
[39]Xiang Junhua,Zhang Yulin.A Coordinate Control Method for Stationkeeping of Regressive Orbit Regional Coverage Satellite Constellation[A].2006 Chinese Control Conference[C],Harbin,China.7-11 Aug.2006.Ⅰ:406-409.
[40]K(o∣¨)nigsmann HJ,Collins JT,Dawson S et al.Autonomous Orbit Maintenance System[J]Acta Astronautica,1996,39:977-985.
[41]Thomas Schetter,Mark Campbell,Derek Surka.Multiple Agent-Based Autonomy for Satellite Constellations[J].Artificial Intelligence,2003.145:147-180.
[42]Wertz JR,Collins JT,Koenigsmann J et al.,Autonomous Constellation Maintenance[A],IAF Workshop on Satellite Constellations[C],18-19 Nov.1997,Toulouse,France.
[43]Collins JT,Dawson S,Wertz JR.Autonomous Constellation Maintenance System[A],Presented.at the 10th Annual AIAA/Utah State University Small Satellite Conference[C],Logan UT,15-19 Sept.1994.
[44]Shah NH.Automated Station-Keeping for Satellite Constellations[M],Master of Science Thesis,MIT,Cambridge,MA.Sept.1997.
[45]于小红,冯书兴.区域观察小卫星星座重构方法研究[J].宇航学报,Apr.2003.24(2):168-172.
[46]张雅声,张育林.性能修复型星座快速重构方法研究[J].装备指挥技术学院学报,Aug.2005,16(4):66-72.
[47]Clifford W.Kelley.Specifications and Management of a 30 Satellite Constellation[A].ION GPS-98,Proceedings of the 11th International Technical Meeting of the Satellite Division of the Institute of Navigation[C],Nashville,TN;US;15-18 Sept.1998.1111-1118.
[48]Park Chan-Wang.Coverage Analysis in Case of Faults of Some Satellites in Low Earth Orbit Satellite Constellations[A].SSC-98-Ⅻ-5,12th AIAA/USU Conference on Small Satellite[C].Logan,UT,1998.
[49]Xiang Junhua,Zhang Yulin.Design and Simulation of Autonomous Fault Diagnosis and Reconfiguration Control System for Satellite Constellation based on Distributed Control Architecture[A].DCABES 2006 PROCEEDINGS[C],Hangzhou,China,12-15 Oct.2006.Ⅰ:970-974.
[50]Drake JH.GPS Constellation Transition to Three Planes and Drifting Ground Tacks[A].ION NTM 2003[C],22-24 Jan.2003,Anaheim,CA.494-503.
[51]Olivier L.de Weck,Uriel Scialomy,Afreen Siddiqi.Optimal Reconfiguration of Satellite Constellations with the Auction Algorithm[A]AIAA 2004-3162,22nd AIAA International Communications Satellite Systems Conference & Exhibit[C], 9-12 May 2004, Monterey,CA.
[52] Siddiqi A, Mellein J, Olivier L.de Weck. Optimal Reconfigurations for Increasing Capacity of Communication Satellite Constellations[A]. AIAA 2005-2065, 46th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics&MaterialsConferenc[C],18-21 Apr. 2005,Austin, Texas.
[53] Walker JG. Some Circular Orbit Patterns Providing Continuous Whole Earth Coverage[J].Journal of the British Interplanetary Society, 1971, 24:369-384.
[54] Walker JG. Continuous Whole Earth Coverage by Circular Orbit Satellites Patterns[R].Royal Aircraft Establishment, Farnborough, UK, TR77044, Mar. 1977.
[55] Hanson JM, Linden Alexander N. Improved Low-Altitude Constellation Design Methods[J].Journal of Guidance, Control and Dynamics, 1989,12:228-236.
[56] Luders RD. Satellite Networks for Continuous Zonal Coverage[J], American Rocket Society Journal, 1961,131:179-184.
[57] Kantsiper Brian, Drake Howard, Using Tessellations for Larger Constellation Design[A],Proceedings of the AAS/AIAA Astrodynamics Conference[C], Girdwood , AK. 16-19, Aug.1999.225-244.
[58] Draim JE. Three- and Four-Satellite Continuous-Coverage Constellation[J], Journal of Guidance, Control and Dynamics, 1985. 8(6):725-730.
[59] Draim JE. A Common-Period Four-Satellite Continuous Global Coverage Constellation[J],Journal of Guidance, Control and Dynamics, 1987.10(5):492-499.
[60] Ronald Proulx, Smith JE, Draim JE et al., ELLIPSOTM GEAR ARRAY Coordinated Elliptical/Circular Constellation[A]. AIAA 98-4383, AIAA/AAS Astrodynamics Specialist Conference[C], 10-12 Aug. 1998.1-18.
[61] Lang Thomas J. Symmetric Circular Orbit Satellite Constellations for Continuous Global Coverage[A]. Proceedings of the AAS/AIAA Astrodynamics Conferenc[C], Kalispell, MT.100-13 Aug. 1987. 1111-1132.
[62] Asvial M, Tafazolli R, Evans BG. Genetic Hybrid Satellite Constellation Design[A]. AIAA 2003-2283, 21st International Communications Satellite Systems Conference and Exhibit[C],Yokohama, Japan, Apr. 15-19,2003.
[63] Brochet C, Enjalbert JM, Garcia JM. A Multiobjective Optimization Approach for the Design of Walker Constellation[A]. 50th International Astronautical Congress[C],Amsterdam, Netherlands, 4-8 Oct. 1999.
[64] Ely TA, Crossley WA, Williams EA. Satellite Constellation Design for Zonal Coverage Using Genetic Algorithms[A]. Proceedings of the AAS/AIAA Space Flight Mechanics Meeting, Monterey[C], CA. 9-11 Feb. 1998.443-460.
[65] Confessore G, Gennaro MD, Ricciarelli S. A Genetic Algorithm to Design Satellite Constellation for the Regional Coverage[A]. Operations Research Proceedings 2000[C],Dresden, September 9-12,2000.
[66] Williams EA, Crossley WA, Lang TJ, Average and Maximum Revisit Time Trade Studies for Satellite Constellations Using a Multiobjective Genetic Algorithm[J]. Journal of Astronautical Sciences, 2001. 49(3):385-400.
[67] Crossley WA, Williams EA. Simulated Annealing and Genetic Algorithm Approaches for Discontinuous Coverage Satellite Constellation Design[J]. Eng. Optim., 2000. 32:353-371.
[68]Enguerran Grandchamp,Vincent Charvillat.Metaheuristics to Deisgn Satellite Constellation[A],4th Metaheuristics International Conference[C],Porto,Portugal,16-20 Jul.2001.505-510.
[69]Frayssinhes E.Investigating New Satellites Constellations Geometries With Genetic Algorithms[A],AIAA 96-3636,Proceedings of the AIAA/AAS Specialist Conference[C],San Diego,CA.Jul.1996.582-589.
[70]George E.Optimization of Satellite Constellations for Discontinuous Global Coverage via Genetic Algorithms[A].AAS 97-621,AAS/AIAA Astrodynamics Specialist Conference[C],Sun Valley,ID.4-7 Aug.1997.
[71]Theresa W.Beech,Stefania Cornara,Miguel Belló Mora.A Study of Three Satellite Constellation Design Algorithms[J].RBCM-J.of the Braz.Soc.Mechanical Sciences,1999.ⅩⅪ(S):19-31.
[72]Monseco EH,Garcia AM,Romay Merino MM.ELCANO:Constellation Design Tool[A].Proceedings of the IAIN World Congress in association with the U.S.ION Annual Meeting[C],San Diego,CA,26-28 June 2000.
[73]Matossian MG.Distributed Task Constellation Design Optimization - An Operations Research Approach to Earth Observing System Configuration Design[A].IAF 47th International Astronautical Congress[C],Beijing,China,7-11 Oct.1996.
[74]Matossian MG.Earth Observing System Constellation Design Optimization Through Mixed Integer Programming[A].The Sixth Alumni Conference of the International Space University[C].1997,158-171.
[75]Amata GB,Fasano G,Arcaro L.Multidisciplinary Optimisation in Mission Analysis and Design Process[R],GPS Programme Ref:GSP 03/N 16.http://www.esa.int/act.
[76]Ellen RT.Evaluation of Multidisciplinary Design Optimization Techniques as Applied to the Spacecraft Design Process[D].PhD Dissertion,University of Colorado at Boulder,1999.
[77]Budianto JO.A Collaborative Optimization Approach to Design and Deployment of a Space Based Infrared System Constellation[A].2000 IEEE Aerospace Conferenc[C],Big Sky,MT.18-25 Mar.2000.
[78]Cyrus DJ.A Multiobjective,Multidisciplinary Design Optimization Methodology for the Conceptual Design of Distributed Satellite System[D],PhD Dissertion,MIT,May 2002.
[79]连全斌,张乃通,张中兆.地带性覆盖星座通用优化设计方法研究[J].高技术通讯,2001.5.54-59
[80]王瑞,马兴瑞,李明.采用遗传算法进行区域覆盖卫星星座优化设计[J].宇航学报,2002,23(3):24-28.
[81]陈琪锋,戴金海.卫星星座系统多学科设计优化研究[J].宇航学报,2003,24(5):502-509.
[82]范丽,张育林.强约束条件下星座一体化优化设计方法研究[J].宇航学报,2006,27(4):779-782.
[83]Sabol C.Application of Sun-Synchronous Critically Inclined Orbits to Global Personal Communications Systems[M].MS Thesis,MIT,Cambridge,MA,November 1994.
[84]Sabol C,Cefola PJ,Metzinger RW.Application of Sun-Synchronous Critically Inclined Orbits to Global Personal Communications Systems[A].AAS 95-222,AAS/AIAA Spaceflight Mechanics Conference[C],Albuquerque,New Mexico,Feb.1995.
[85]Sabol C,Draim J,Cefola PJ.Refinment of a Sun-Synchronous,Critically Inclined Orbit for the Ellipso Personal Communications Systems[J].The Journal of Astronautical Sciences, Oct.-Dec.1996.44(4):467-489.
[86]Kaplan E.D著,邱致和,王万义译.GPS原理与应用[M].北京:电子工业出版社,2004.6.
[87]Antony G W,Harding W,Hagemeier H.Assessment of Responsive Replenishment Launch for Constellation Management[A].AIAA 99-4615,AIAA Space Technology Conference and Exposition[C],Albuquerque,NM,28-30 Sept.1999.
[88]Paul Massatt,Fred Fritzen.Assessment of the Proposed GPS 27-Satellite Constellation[A].ION GPS/GNSS 2003[C],Portland OR,9-12 Sept.2003,399-406.
[89]项军华,张育林.基于卫星可靠度和MTTR星座空间备份策略优化设计[J].系统工程与电子技术.Sep.2007,29(9):1576-1580.
[90]Olivier de Weck,Richard de Neufville,Mathieu Chaize.Staged Deployment of Communications Satellite Constellations in Low Earth Orbit[J].Journal of Aerospace Computing,Information,and Communication,March 2004.(1):119-136.
[91]Olivier L.de Weck,Richard de Neufville,Mathieu Chaize.Enhancing the Economics of Communications Satellite via Orbital Reconfigurations and Staged Deployment[A].AIAA 2003-6317,Space 2003[A],Long Beach,California.23-25 Sept.2003.
[92]Mathieu Chaize.Enhancing the Economics of Satellite Constellations via Staged Deployment and Orbital Reconfiguration[M],Master of Science,MIT,May,2005.
[93]Serena Chan,Samuels AB,Shah NB et al.Optimization of Hybrid Satellite Constellations using Multiple Layers and Mixed Circular-Elliptical Orbits[A].AIAA 2004-3205.22nd AIAA International Communications Satellite Systems Conferenc&Exhibit[C],Monterey,CA,9-12 May 2004.
[94]Romay-Merino MM,Pulido Cobo JA,Herraiz-Monseco E.Design of High Performance and Cost Efficient Constellations for a Future Global Navigation Satellite System[A].ION GPS'98,Proceedings of the 11th International Meeting of the Satellite Division of the Institute of Navigation[C],Nashville,TN,15-18 Sept.1998.1085-1095.
[95]Sam Pullen,Bradford Parkinson.Optimal Augmentation of GPS using Inexpensive Geosynchronous Navigation Satellites[A].Proceedings of the ION GPS 97[C],Sept.1997.
[96]Chang-Hee Won,Ja-Young Kang,Jong Won Eun et al.,Feasibility Study of Augmentation and Backup Navigation Systems in Asia-Pacific Region[A].ION GPS'99[C],Nashville,TN.14-17 Sept.1999.2131-2137.
[97]周其焕,黄建宇,全球卫星导航系统的近期进展[J].中国民航学院学报.Aug.2000.18(4):53-59.
[98]Rafael Lucas,Alberto Garcial,Steve Abbondanza.Galileo Constellation:Optimisation Criteria and Achievements[A].GNSS 2001[C],Serville.Spain.2001.
[99]Gatti G,Garutti A,Mandorlo G et al,The GIOVE-A Satellite:From Design to in-orbit Commissioning[A].Proc.ION GNSS 2006[C],Fort Worth,TX,September 2006.
[100]杨维廉,近圆轨道控制的分析方法[J],中国空间科学技术,2003.10.(5):1-5.
[101]Shah NH,Proulx RJ,Brian Kantsiper et al.Automated Station-Keeping for Satellite Constellations[A].AAS 97-623.Proceedings of the AAS/AIAA Astrodynamics Conference[C],Sun Valley,Idaho,August 1997;Advances in Astronautical Sciences.97(1):357-385.
[102]Bruno MJ,Pernicka HJ.Tundra Constellation Design and Stationkeeping[J],Journal of Spacecraft and Rockets,2005.42(5):902-1003.
[103]项军华,张育林.区域覆盖星座构型优化及协同控制策略研究[J],飞行力学,Sep.2007,25(3):87-91.
[104]Castiel D,Brosius JW,Draim JE.EllipsoTM:Coverage Optimization Using Elliptic Orbits[A].AIAA 94-1098.15th AIAA International Communications Satellite Systems Conference[C],SanDiego CA,February-March 1994.Technical Papers.Pt.3(A94-2265105-32),Washington,DC,American Institute of Aeronautics and Astronautics,1994.1235-1241.
[105]Kyle O'Keefe.Availability and Reliability Advantages of GPS/Galileo Integration[A].Proceedings of ION GPS 2001,Session C4[C],Salt Lake City,UT,11-14 Sep.2001.2096-2104.
[106]Manop A,Yoshi H,Phil P.Autonomous Control System for Precise Orbit Maintenance[A].Proceeding of the 14th Annual AIAA/USU Conference on Small Satellite[C],Logan,Utah,24-28 Aug.2001,1-9.
[107]Ricardo Piriz,Belen Martin-Peiro,Miguel Romay-Merino.The Galileo Constellation Design:A Systematic Approach[A].ION GNSS 18th International Technical Meeting of the Satellite Division[C],Long Beach,CA,13-16,Sep,2005.1296-1306.
[108]Zandbergen R,Dinwiddy S,Hahn J et al.Galileo Orbit Selection[A].ION GNSS 17th International Technical Meeting of the Satellite Division[C],Long Beach,CA,21-24 Sept.2004.616-623.
[109]Wertz JR,Larson JW.Space Mission Analysis and Design(Third Edition)[M].Published Jointly by Microcosm Press and Kluwer Academic Publishers,1999.
[110]刘林,航天器轨道理论[M].北京:国防工业出版社,2000.6.
[111]Walker P,Stokes PH,Wilkinson JE et al.Long-Term Collision Risk Prediction for Low Earth Orbit Satellite Constellation[J].Acta Astronautica.2000.47(2-9):707-717.
[112]Xiang Junhua,Zhang Yulin.Research on Design and Control of Spaceborne Multistatic Radar System[A].Proceedings of 2006 CIE International Conference on RADAR[C]Shanghai,China.Oct.16-19,2006.Ⅱ:264-268.
[113]Palmucci P,Pavesi B.Archimedes Mission Aspects[A].IEE Colloquium on Highly Elliptical Orbit Satellite Systems[C].London,UK.24 May 1989,11/1-11/6.
[114]杨维廉.临界倾角与冻结轨道[J].宇航学报.1993.7.(3):1-9.
[115]ftp://ftp.igscb.jpl.nasa.gov.
[116]张艳.基于星间观测的星座自主导航方法研究[D].国防科技大学博士学位论文,2005.9.
[117]赵黎平,周凤岐,周军.实现轨道偏心率协调控制的卫星轨道维持方法[J].西北工业大学学报.Feb.2002.20(1):125-127.
[118]项军华,张育林.卫星姿态控制稳定度对星座构形稳定性的影响研究[J].航天控制,Jun.2007,25(3):43-47.
[119]杨嘉墀.航天器轨道动力学与控制(上)[M].北京:宇航出版社,1995.12.
[120]Wickert DP,Shaw GB,Hastings D.Impact of a Distributed Architecture for Space-Based Radar[J].Journal of Spacecraft and Rockets,Sep.-Oct.1998,35(5):703-713.
[121]Tollefson MV,Preiss BK.Space Based Radar Constellation Optimization[A].Proceedings of Aerospace Conference 1998[C],March 1998.3:379-388.
[122]任萱.人造地球卫星轨道动力学[M].长沙:国防科技大学出版社,1988.
[123]范丽,张育林.同构双基地雷达星座优化设计[J].系统工程与电子技术,Nov.2005. 27(1):1883-1888.
[124]Cornara S,Beech TW,Bello-Mora Met al.Satellite Constellation Launch,Deployment,Replacement and End-Of-Life Strategies[A].SSC99-X-1,13th Annual AIAA/USU Conference on Small Satellite[C],Logan,Utah,23-26 Aug.1999.
[125]Slattery R,Kovach Karl.New and Improved GPS Satellite Constellation Availability Model[A],ION GPS'99[C],Nashville,TN,14-17 Sept.1999.2103-2112
[126]Garrison TP,Ince M,Pizzicaroli J et al.Systems Engineering Trades for the IRIDIUM Constellation[J].ournal of Spacecraft and Rockets,1997.34(5):675-680.
[127]Xie M,Dai Y S,Poh K L.Computing System Reliability:Models and Analysis[M].New York:Kluwer Academic/Plenum Publishers,Apr.2004.
[128]郭齐胜,郅志刚,杨瑞平等.装备效能评估概论[M].北京:国防工业出版社,2005.8.
[129]Brian E.Operations Planning and Formation Flying:Analyzing Resource Usage in Formation Assembly[A].Proceedings of the 13th Annual AIAA/USU Conference on Small Satellites[C].Logan,Utah,23-26 Aug.1999.1-11.
[130]王永澄,付锋,陈晓凤.圆轨道同步卫星在区域导航系统中的应用[J].南京航空航天大学学报,2002,34(4):359-363.
[131]王莉.区域导航卫星系统的星座设计与比较[J].飞行器测控学报,1999.18(4)1-8.
[132]荆武兴.高长生.亚太区域导航八星星座分析[J].航天控制,Jul.2005,23(6):4-8.
[133]胡松杰.卫星星座的动力学研究[D].南京:南京大学博士学位论文,2003.12.
[134]申培萍.全局优化方法[M].北京:科学出版社.2006.3.
[135]徐玖平,李军.多目标决策的理论与方法[M].北京:清华大学出版社.2005.3.
[136]玄光男,程润伟著;于歆杰,周根贵译.遗传算法与工程优化[M].北京:清华大学出版社.2004.1.
[137]郦苏丹,朱江,李广侠.采用遗传算法的中轨区域通信星座优化设计[J].系统仿真学报,Jun.2005.17(6):1366-1369.
[138]赵勇,颜力,陈小前,王振国.基于MDO方法的月球探测卫星总体设计[J].上海航天,2006.(2):37-41.
[139]徐亚栋,钱林方.复合材料身管热-结构分析与优化[J].弹道学报,Jun.2006.18(2):31-35.
[140]iSIGHT Reference Guide.
[141]Back T.Selective Pressure in Evolutionary Algorithms:a Characterization of Selection Mechanisms[A].Proceedings of the First IEEE Conference on Evolutionary Computation(ICEC94)[C],Orlando,Dlorida,1994.57-62.
[142]Goldberg D,Korb B,Deb K.Messy Genetic Algorithms:Motivation,Analysis,and First Results[J].Complex System,1989.3:493-530.
[143]杨嘉墀.航天器轨道动力学与控制(下)[M].北京:宇航出版社,2001.12.
[144]毛悦,孙付平.利用Walker星座实现全球导航卫星星座设计[J].测绘科学技术学报,Apr.2006,23(2):153-156.
[145]http://www.calt.com/.
[146]范丽,张育林.Walker星座星间链路构建准则及优化设计研究[J].飞行力学,Jun.2007,25(3):93-96.
[147]王振永,王平,顾学迈等.卫星网络中永久星间链路的设计方法研究[J].通信学报,Aug. ?2006, 27(8): 129-33.
[148] Salzwedel KH, Freund H, Schorcht U. Examination of the Circular Polar Satellite Constellation for the Use of Inter-Satellite Links[A], Personal Wireless Communication of 1997 IEEE International Conference[C], Mumbai, India, Dec. 1997.283-287.
[149] Fonseca CM, Fleming PJ. Genetic Algorithms for Multiobjective Optimization: Formulation,Discussion and Generalization[A]. Proceedings of the 5th International Conference on Genetic Algorithms[C], Sam Mateo, CA, Jul. 1993. 416-423.
[150] Horn J, Nafpliotis N. Multiobjective Optimization Using the Niched Pareto Genetic Algorithm[R]. IlliGAL Report 93005, Illinois Genetic Algorithms Laboratory, University of Illinois, Urbana, Champaign, Jul. 1993.
[151] Srinivas N, Deb K. Multiobjective Optimization Using Nondominated Sorting in Genetic Algorithms[J]. Journal of Evolutionary Computation, 1995. 2(3):221-248.
[152] Zitzler E, Thiele L. Multiobjective Evolutionary Algorithm: A Comparative Case Study and the Strength Pareto Approach[J]. IEEE Transactions on Evolutionary Computation, 1999.3(4):257-271.
[153] Zitzler E, Laumanns M, Thiele L. SPEA2: Improving the Strength Pareto Evolutionary Algorithm[R]. TIK-Report 103, Computer Engineering and Networks Laboratory(TIK),Swiss Federal Institute of Technology(ETH), Zurich, Switzerland, May 2001.
[154] Watanabe S, Hiroyasu T, Miki M. Neighborhood Cultivation Genetic Algorithm for Multi-Objective Optimization Problems[A].Proceedings of 4th Asia-Pacific Conference on Simulated Evolution and Learning(SEAL'02)[C], Orchid Country Club, Singapore, Nov.2002.1:198-202.
[155] Deb K, Agrawal S, Pratap A et al. A Fast Elitist Non-Dominated Sorting Genetic Algorithm for Multi-Objective Optimization: NSGA-II[R]. Kanpur Genetic Algorithms Laboratory Report No. 200001. Kanpur Genetic Algorithms Laboratory, Indian Institute of Technology Kanpur, Kanpur India, 2000.
[156] Deb K, Pratap A, Agarwal S et al. A Fast and Elitist Multiobjective Genetic Algorithm:NSGA-II[J]. IEEE Transactions on Evolutionary Computation, Apr. 2002, 6(2):182-197.
[157] Walker JG. Satellite Constellation[J]. Journal of the British Interplanetary Society, 1984,37:559-571.
[158] Adams RJ, Buffmgton JM, Banda SS. Robust, Nonlinear, High Angle-of-Attack Control Design for a Supermaneuverable Vechicle[R]. NTIS No: N9425108/9/HDM.
[159] Adams WS, Rider L. Circular Polar Constellations Providing Continuous Single or Multiple Coverage above a Specified Latitude[J] Journal of Astronautical Science, 1987.35(3):155-192.
[160] Salgado G, Abbondanza S, Blondel R et al. Constellation Availability Concepts for Galileo[A]. ION NTM 2001[C], Long Beach, CA, 22-24 Jan. 2001. 778-786.
[2]Thunnissen DP,Balancing Cost,Risk,and Performance Under Uncertainty in Preliminary Mission Design[A].AIAA 2004-5878,Space 2004 Conference and Exhibit[C],San Diego,CA,28-30 Sept.2004.
[3]Kelley CW.Minimizing the cost of availability of services from a constellation of satellites[D].Ph.D Thesis,University of Southern California,Los Angles,CA,2003.
[4]项军华,张育林.卫星星座的自主位置保持[A].全国第十一届空间及运动体控制技术学术会议[C],云南昆明,2004.8,215-220.
[5]Martin Peiro AB,Beech TW,Alvaro Mozo Garcia et al.Galileo In-Orbit Control Strategy[A].Proceedings of the IAIN World Congress in association with the U.S.ION Annual Meeting[C],26-28,Jun.,2000,San Diego,CA.,469-480.
[6]Wertz JR,Gwynne Gurevich.Applications of Autonomous On-Board Orbit Control[A],11th AAS/AIAA Space Flight Mechanics Meeting[C],Santa Barbara,CA,11 - 15 Feb.2001.
[7]Walt Truszkowsk,David Zoch,Dan Smith.Autonomy for Constellations[Z].http://agents.gsfc.nasa.gov/papers/index.html.
[8]Ananda MP,Bernstein H,Cunningham KE et al.,Global Position System(GPS)Autonomous Navigation[J].Inst.of Electrical and Electronics Engineer Position Location and Navigation Symposium,Inst.of Electrical and Electronics Engineers,New York,1990.
[9]Swan PA.A Revolution in Progress:IRIDIUM LEO Operations.AIAA-97-3954.AIAA Defense and Space Programs Conference and Exhibit - Critical Defense and Space Programs for the Future,Huntsville,AL;UNITED STATES;23-25 Sept.1997.158-163.1997.
[10]John Tandler.Automating the Operations of the ORBCOMM Constellation[A].10th Annual AIAA/Utah State University Conference on Small Satellites[C],North Logan,UT.Sept.1996.
[11]Andrew W.Lewin.Low-Cost Operation of the ORBCOMM Satellite Constellation[J].Journal of Reducing Space Mission Cost.Mar.1998.1(1):105-117.
[12]Clifford W.Kelley,Transition to a 30 Satellite GPS Constellation[A].Proceedings ION NTM 1998[C],Jan.1998.371-380.
[13]Clifford W.Kelley,Steven C.Fisher.Orbital Optimization of the GPS Constellation and Its Effect on Accuracy and Availability[A].Proceeding of ION GPS-97[C],Sept.16-19,1997,Kansas City,MO.423-435.
[14]Turner AE,Rodden JJ,Melvin T et al.,GlobalStarTM Constellation Design and Establishment Experience[A].AAS/AIAA Astrodynamics Conference Advances in the Astronautical Sciences[C],MT,US,August 3-7,2003.116(3):2127-2143.
[15]范丽.卫星星座一体化优化设计研究[D].国防科技大学博士学位论文,2006.3.
[16]Olivier De Wech,Richard de Neufville,Mathieu Chaize et al.,Enhancing the Economics of Satellite Constellation via Staged Deployment[P].International Telecommunications Union Strategy and Policy Unit,Geneva,1 July 2004.
[17]Lefebvre L,Lamy A,Brousse P et al.Relative Station Keeping Optimization for the Starsys Constellation[A],Proceedings of the 12th International Symposium on Space Flight Dynamics[C],ESOC,Darmstadt.Germany.2-6 Jun.1997.
[18]张洪华,李鸿铭,邹广瑞,李昕.圆轨道星座位置保持控制的仿真与研究[J].中国空间科学技术,(6):15-23.2000.12.
[19]张晓敏.航天器相对轨道动力学与控制研究[D].北京航空航天大学博士学位论文,2000.
[20]Dong-Woo Gim,Kyle T.Alfriend.The State Transition Matrix of Relative Motion for the Perturbed Non-circular Reference Orbit[A].AAS 01-222,AAS/AIAA Space Flight Mechanics Meeting[C],11-15 Feb.2001,San Diego,CA.1-23.
[21]Chao CC,Bowen AF.Effects of Long-term Orbit Perturbations and Injection errors on GPS Constellation Values[A].AIAA 86-2173,Astrodynamics Conference[C],August 18-20,1986,Williamsburg,VA.
[22]胡松杰,陈力,刘林.卫星星座的结构演化[J].天文学报,Feb.,2003,44(1):46-54.
[23]Deleflie F,Legendre P,Exertier P et al.,Long Term Evolution of the Galileo Constellation due to Gravitation Forces[J].Advances in Space Research,2005,36:402-411.
[24]Marek Ziebart,Sima Adhya.GPS Block ⅡR Non-Conservative Force Modelling:Computation and Implications[A].ION GPS/GNSS 2003[C],Portland,OR.9-12 Sept.2003.2671-2678.
[25]Marek Ziebart,Sima Adhya,Ant Sibthorpe et al.Taking the Long View:The Impact of Spacecraft Structural Design and Hign Precision Force Modeling on Long-term Orbit Evolution[A].ION GPS/GNSS 2003[C],Portland,OR.9-12 Sept.2003,1002-1008.
[26]Chao CC.Long-Term Orbit Perturbation of the Draim Four-Satellite Constellation[J].AIAA 90-2900,AIAA/AAS Astrodynamics Conference,Portland,OR,Aug 20-22,1990.Technical Papers.Pt.1(A90-52957 24-13).Washington,DC,American Institute of Aeronautics and Astronautics,1990.208-213.
[27]Schutz BE,Craig DE.GPS Orbit Evolution:1998-2000[A].AIAA 2000-4237,AIAA/AAS Astrodynamics Specialist Conference[C],Denver,CO.14-17,Aug.2000.
[28]Lamy A,Pascal S.Station Keeping Strategies for Constellations of Satellites[J],Spaceflight Dynamics,1993.84:819-833.
[29]Brodsky P,Chen S M-S.Automatic Maneuver Planning for Maintenance of Satellite Constellation Geometry[A]In:Flight Mechanics Symposium 1997[C],Greenbelt,MD,19-21 May 1997.397-404.
[30]Glickman RE.TIDE:The Timed-Destination Approach to Constellation Formationkeeping,[A]AAS 94-122,In:Spaceflight Mechanics 1994;Proceedings of the 4th AAS/AIAA Spaceflight Mechanics Meeting[C],Cocoa Beach,FL,14-16 Feb.,1994.
[31]Ulybyshev U.Long-Term Formation Keeping of Satellite Constellation Using Linear-Quadratic Controller[J].Journal of Guidance,Control,and Dynamics,1998,21(1),109-115.
[32]Lasserre E,Dufour F,Bernussou et al.A Linear Programming Solution to the Homogeneous Satellite Constellation StationKeeping[A].IA9-97-A.4.08,48th International Astronautical Congress[C],Turin,Italy,6-10 Oct.,1997.
[33]McInnes CR.Autonomous Ring Formation for a Planar Constellation of Satellites[J].Journal of Guidance,Control,and Dynamics,Oct.1995,18(5):1215-1217.
[34]Evandro Marconi Rocco Marcelo,Lopes de Oliveira e Souza Antonio,Fernando Bertachini de Almeida Prado.Multi-Objective Optimization Approach Applied to StationKeeping of Satellite Constellations[A],AAS/AIAA Astrodynamics Conference[C],Jul.30-Aug.2,2001,Quebec City,Quebec,Canada.
[35]向开恒,卫星星座站位保持与控制研究[D],北京航空航天大学博士学位论文,1999.
[36]Randal Beard.Architecture and Algorithms for Constellation Control[R].Final Report,Brigham Young University,16 Mar.1998.
[37]Jean-Louis Calvet,Ghita Kardoudi.A Multilevel Approach for the Station-keeping of a Phased Satellite Constellation[A],13th Triennial World Congress[C],San Francisco,USA.
[38]Rondinelli G,Cramarossa A,Graziani F.Orbit Control Strategy for a Constellation of Three Satellites in Tundra Orbits[A].AAS 89-411,AAS/AIAA Astrodynamics Specialist Conference[C],7-10 Aug.1989.1-13.
[39]Xiang Junhua,Zhang Yulin.A Coordinate Control Method for Stationkeeping of Regressive Orbit Regional Coverage Satellite Constellation[A].2006 Chinese Control Conference[C],Harbin,China.7-11 Aug.2006.Ⅰ:406-409.
[40]K(o∣¨)nigsmann HJ,Collins JT,Dawson S et al.Autonomous Orbit Maintenance System[J]Acta Astronautica,1996,39:977-985.
[41]Thomas Schetter,Mark Campbell,Derek Surka.Multiple Agent-Based Autonomy for Satellite Constellations[J].Artificial Intelligence,2003.145:147-180.
[42]Wertz JR,Collins JT,Koenigsmann J et al.,Autonomous Constellation Maintenance[A],IAF Workshop on Satellite Constellations[C],18-19 Nov.1997,Toulouse,France.
[43]Collins JT,Dawson S,Wertz JR.Autonomous Constellation Maintenance System[A],Presented.at the 10th Annual AIAA/Utah State University Small Satellite Conference[C],Logan UT,15-19 Sept.1994.
[44]Shah NH.Automated Station-Keeping for Satellite Constellations[M],Master of Science Thesis,MIT,Cambridge,MA.Sept.1997.
[45]于小红,冯书兴.区域观察小卫星星座重构方法研究[J].宇航学报,Apr.2003.24(2):168-172.
[46]张雅声,张育林.性能修复型星座快速重构方法研究[J].装备指挥技术学院学报,Aug.2005,16(4):66-72.
[47]Clifford W.Kelley.Specifications and Management of a 30 Satellite Constellation[A].ION GPS-98,Proceedings of the 11th International Technical Meeting of the Satellite Division of the Institute of Navigation[C],Nashville,TN;US;15-18 Sept.1998.1111-1118.
[48]Park Chan-Wang.Coverage Analysis in Case of Faults of Some Satellites in Low Earth Orbit Satellite Constellations[A].SSC-98-Ⅻ-5,12th AIAA/USU Conference on Small Satellite[C].Logan,UT,1998.
[49]Xiang Junhua,Zhang Yulin.Design and Simulation of Autonomous Fault Diagnosis and Reconfiguration Control System for Satellite Constellation based on Distributed Control Architecture[A].DCABES 2006 PROCEEDINGS[C],Hangzhou,China,12-15 Oct.2006.Ⅰ:970-974.
[50]Drake JH.GPS Constellation Transition to Three Planes and Drifting Ground Tacks[A].ION NTM 2003[C],22-24 Jan.2003,Anaheim,CA.494-503.
[51]Olivier L.de Weck,Uriel Scialomy,Afreen Siddiqi.Optimal Reconfiguration of Satellite Constellations with the Auction Algorithm[A]AIAA 2004-3162,22nd AIAA International Communications Satellite Systems Conference & Exhibit[C], 9-12 May 2004, Monterey,CA.
[52] Siddiqi A, Mellein J, Olivier L.de Weck. Optimal Reconfigurations for Increasing Capacity of Communication Satellite Constellations[A]. AIAA 2005-2065, 46th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics&MaterialsConferenc[C],18-21 Apr. 2005,Austin, Texas.
[53] Walker JG. Some Circular Orbit Patterns Providing Continuous Whole Earth Coverage[J].Journal of the British Interplanetary Society, 1971, 24:369-384.
[54] Walker JG. Continuous Whole Earth Coverage by Circular Orbit Satellites Patterns[R].Royal Aircraft Establishment, Farnborough, UK, TR77044, Mar. 1977.
[55] Hanson JM, Linden Alexander N. Improved Low-Altitude Constellation Design Methods[J].Journal of Guidance, Control and Dynamics, 1989,12:228-236.
[56] Luders RD. Satellite Networks for Continuous Zonal Coverage[J], American Rocket Society Journal, 1961,131:179-184.
[57] Kantsiper Brian, Drake Howard, Using Tessellations for Larger Constellation Design[A],Proceedings of the AAS/AIAA Astrodynamics Conference[C], Girdwood , AK. 16-19, Aug.1999.225-244.
[58] Draim JE. Three- and Four-Satellite Continuous-Coverage Constellation[J], Journal of Guidance, Control and Dynamics, 1985. 8(6):725-730.
[59] Draim JE. A Common-Period Four-Satellite Continuous Global Coverage Constellation[J],Journal of Guidance, Control and Dynamics, 1987.10(5):492-499.
[60] Ronald Proulx, Smith JE, Draim JE et al., ELLIPSOTM GEAR ARRAY Coordinated Elliptical/Circular Constellation[A]. AIAA 98-4383, AIAA/AAS Astrodynamics Specialist Conference[C], 10-12 Aug. 1998.1-18.
[61] Lang Thomas J. Symmetric Circular Orbit Satellite Constellations for Continuous Global Coverage[A]. Proceedings of the AAS/AIAA Astrodynamics Conferenc[C], Kalispell, MT.100-13 Aug. 1987. 1111-1132.
[62] Asvial M, Tafazolli R, Evans BG. Genetic Hybrid Satellite Constellation Design[A]. AIAA 2003-2283, 21st International Communications Satellite Systems Conference and Exhibit[C],Yokohama, Japan, Apr. 15-19,2003.
[63] Brochet C, Enjalbert JM, Garcia JM. A Multiobjective Optimization Approach for the Design of Walker Constellation[A]. 50th International Astronautical Congress[C],Amsterdam, Netherlands, 4-8 Oct. 1999.
[64] Ely TA, Crossley WA, Williams EA. Satellite Constellation Design for Zonal Coverage Using Genetic Algorithms[A]. Proceedings of the AAS/AIAA Space Flight Mechanics Meeting, Monterey[C], CA. 9-11 Feb. 1998.443-460.
[65] Confessore G, Gennaro MD, Ricciarelli S. A Genetic Algorithm to Design Satellite Constellation for the Regional Coverage[A]. Operations Research Proceedings 2000[C],Dresden, September 9-12,2000.
[66] Williams EA, Crossley WA, Lang TJ, Average and Maximum Revisit Time Trade Studies for Satellite Constellations Using a Multiobjective Genetic Algorithm[J]. Journal of Astronautical Sciences, 2001. 49(3):385-400.
[67] Crossley WA, Williams EA. Simulated Annealing and Genetic Algorithm Approaches for Discontinuous Coverage Satellite Constellation Design[J]. Eng. Optim., 2000. 32:353-371.
[68]Enguerran Grandchamp,Vincent Charvillat.Metaheuristics to Deisgn Satellite Constellation[A],4th Metaheuristics International Conference[C],Porto,Portugal,16-20 Jul.2001.505-510.
[69]Frayssinhes E.Investigating New Satellites Constellations Geometries With Genetic Algorithms[A],AIAA 96-3636,Proceedings of the AIAA/AAS Specialist Conference[C],San Diego,CA.Jul.1996.582-589.
[70]George E.Optimization of Satellite Constellations for Discontinuous Global Coverage via Genetic Algorithms[A].AAS 97-621,AAS/AIAA Astrodynamics Specialist Conference[C],Sun Valley,ID.4-7 Aug.1997.
[71]Theresa W.Beech,Stefania Cornara,Miguel Belló Mora.A Study of Three Satellite Constellation Design Algorithms[J].RBCM-J.of the Braz.Soc.Mechanical Sciences,1999.ⅩⅪ(S):19-31.
[72]Monseco EH,Garcia AM,Romay Merino MM.ELCANO:Constellation Design Tool[A].Proceedings of the IAIN World Congress in association with the U.S.ION Annual Meeting[C],San Diego,CA,26-28 June 2000.
[73]Matossian MG.Distributed Task Constellation Design Optimization - An Operations Research Approach to Earth Observing System Configuration Design[A].IAF 47th International Astronautical Congress[C],Beijing,China,7-11 Oct.1996.
[74]Matossian MG.Earth Observing System Constellation Design Optimization Through Mixed Integer Programming[A].The Sixth Alumni Conference of the International Space University[C].1997,158-171.
[75]Amata GB,Fasano G,Arcaro L.Multidisciplinary Optimisation in Mission Analysis and Design Process[R],GPS Programme Ref:GSP 03/N 16.http://www.esa.int/act.
[76]Ellen RT.Evaluation of Multidisciplinary Design Optimization Techniques as Applied to the Spacecraft Design Process[D].PhD Dissertion,University of Colorado at Boulder,1999.
[77]Budianto JO.A Collaborative Optimization Approach to Design and Deployment of a Space Based Infrared System Constellation[A].2000 IEEE Aerospace Conferenc[C],Big Sky,MT.18-25 Mar.2000.
[78]Cyrus DJ.A Multiobjective,Multidisciplinary Design Optimization Methodology for the Conceptual Design of Distributed Satellite System[D],PhD Dissertion,MIT,May 2002.
[79]连全斌,张乃通,张中兆.地带性覆盖星座通用优化设计方法研究[J].高技术通讯,2001.5.54-59
[80]王瑞,马兴瑞,李明.采用遗传算法进行区域覆盖卫星星座优化设计[J].宇航学报,2002,23(3):24-28.
[81]陈琪锋,戴金海.卫星星座系统多学科设计优化研究[J].宇航学报,2003,24(5):502-509.
[82]范丽,张育林.强约束条件下星座一体化优化设计方法研究[J].宇航学报,2006,27(4):779-782.
[83]Sabol C.Application of Sun-Synchronous Critically Inclined Orbits to Global Personal Communications Systems[M].MS Thesis,MIT,Cambridge,MA,November 1994.
[84]Sabol C,Cefola PJ,Metzinger RW.Application of Sun-Synchronous Critically Inclined Orbits to Global Personal Communications Systems[A].AAS 95-222,AAS/AIAA Spaceflight Mechanics Conference[C],Albuquerque,New Mexico,Feb.1995.
[85]Sabol C,Draim J,Cefola PJ.Refinment of a Sun-Synchronous,Critically Inclined Orbit for the Ellipso Personal Communications Systems[J].The Journal of Astronautical Sciences, Oct.-Dec.1996.44(4):467-489.
[86]Kaplan E.D著,邱致和,王万义译.GPS原理与应用[M].北京:电子工业出版社,2004.6.
[87]Antony G W,Harding W,Hagemeier H.Assessment of Responsive Replenishment Launch for Constellation Management[A].AIAA 99-4615,AIAA Space Technology Conference and Exposition[C],Albuquerque,NM,28-30 Sept.1999.
[88]Paul Massatt,Fred Fritzen.Assessment of the Proposed GPS 27-Satellite Constellation[A].ION GPS/GNSS 2003[C],Portland OR,9-12 Sept.2003,399-406.
[89]项军华,张育林.基于卫星可靠度和MTTR星座空间备份策略优化设计[J].系统工程与电子技术.Sep.2007,29(9):1576-1580.
[90]Olivier de Weck,Richard de Neufville,Mathieu Chaize.Staged Deployment of Communications Satellite Constellations in Low Earth Orbit[J].Journal of Aerospace Computing,Information,and Communication,March 2004.(1):119-136.
[91]Olivier L.de Weck,Richard de Neufville,Mathieu Chaize.Enhancing the Economics of Communications Satellite via Orbital Reconfigurations and Staged Deployment[A].AIAA 2003-6317,Space 2003[A],Long Beach,California.23-25 Sept.2003.
[92]Mathieu Chaize.Enhancing the Economics of Satellite Constellations via Staged Deployment and Orbital Reconfiguration[M],Master of Science,MIT,May,2005.
[93]Serena Chan,Samuels AB,Shah NB et al.Optimization of Hybrid Satellite Constellations using Multiple Layers and Mixed Circular-Elliptical Orbits[A].AIAA 2004-3205.22nd AIAA International Communications Satellite Systems Conferenc&Exhibit[C],Monterey,CA,9-12 May 2004.
[94]Romay-Merino MM,Pulido Cobo JA,Herraiz-Monseco E.Design of High Performance and Cost Efficient Constellations for a Future Global Navigation Satellite System[A].ION GPS'98,Proceedings of the 11th International Meeting of the Satellite Division of the Institute of Navigation[C],Nashville,TN,15-18 Sept.1998.1085-1095.
[95]Sam Pullen,Bradford Parkinson.Optimal Augmentation of GPS using Inexpensive Geosynchronous Navigation Satellites[A].Proceedings of the ION GPS 97[C],Sept.1997.
[96]Chang-Hee Won,Ja-Young Kang,Jong Won Eun et al.,Feasibility Study of Augmentation and Backup Navigation Systems in Asia-Pacific Region[A].ION GPS'99[C],Nashville,TN.14-17 Sept.1999.2131-2137.
[97]周其焕,黄建宇,全球卫星导航系统的近期进展[J].中国民航学院学报.Aug.2000.18(4):53-59.
[98]Rafael Lucas,Alberto Garcial,Steve Abbondanza.Galileo Constellation:Optimisation Criteria and Achievements[A].GNSS 2001[C],Serville.Spain.2001.
[99]Gatti G,Garutti A,Mandorlo G et al,The GIOVE-A Satellite:From Design to in-orbit Commissioning[A].Proc.ION GNSS 2006[C],Fort Worth,TX,September 2006.
[100]杨维廉,近圆轨道控制的分析方法[J],中国空间科学技术,2003.10.(5):1-5.
[101]Shah NH,Proulx RJ,Brian Kantsiper et al.Automated Station-Keeping for Satellite Constellations[A].AAS 97-623.Proceedings of the AAS/AIAA Astrodynamics Conference[C],Sun Valley,Idaho,August 1997;Advances in Astronautical Sciences.97(1):357-385.
[102]Bruno MJ,Pernicka HJ.Tundra Constellation Design and Stationkeeping[J],Journal of Spacecraft and Rockets,2005.42(5):902-1003.
[103]项军华,张育林.区域覆盖星座构型优化及协同控制策略研究[J],飞行力学,Sep.2007,25(3):87-91.
[104]Castiel D,Brosius JW,Draim JE.EllipsoTM:Coverage Optimization Using Elliptic Orbits[A].AIAA 94-1098.15th AIAA International Communications Satellite Systems Conference[C],SanDiego CA,February-March 1994.Technical Papers.Pt.3(A94-2265105-32),Washington,DC,American Institute of Aeronautics and Astronautics,1994.1235-1241.
[105]Kyle O'Keefe.Availability and Reliability Advantages of GPS/Galileo Integration[A].Proceedings of ION GPS 2001,Session C4[C],Salt Lake City,UT,11-14 Sep.2001.2096-2104.
[106]Manop A,Yoshi H,Phil P.Autonomous Control System for Precise Orbit Maintenance[A].Proceeding of the 14th Annual AIAA/USU Conference on Small Satellite[C],Logan,Utah,24-28 Aug.2001,1-9.
[107]Ricardo Piriz,Belen Martin-Peiro,Miguel Romay-Merino.The Galileo Constellation Design:A Systematic Approach[A].ION GNSS 18th International Technical Meeting of the Satellite Division[C],Long Beach,CA,13-16,Sep,2005.1296-1306.
[108]Zandbergen R,Dinwiddy S,Hahn J et al.Galileo Orbit Selection[A].ION GNSS 17th International Technical Meeting of the Satellite Division[C],Long Beach,CA,21-24 Sept.2004.616-623.
[109]Wertz JR,Larson JW.Space Mission Analysis and Design(Third Edition)[M].Published Jointly by Microcosm Press and Kluwer Academic Publishers,1999.
[110]刘林,航天器轨道理论[M].北京:国防工业出版社,2000.6.
[111]Walker P,Stokes PH,Wilkinson JE et al.Long-Term Collision Risk Prediction for Low Earth Orbit Satellite Constellation[J].Acta Astronautica.2000.47(2-9):707-717.
[112]Xiang Junhua,Zhang Yulin.Research on Design and Control of Spaceborne Multistatic Radar System[A].Proceedings of 2006 CIE International Conference on RADAR[C]Shanghai,China.Oct.16-19,2006.Ⅱ:264-268.
[113]Palmucci P,Pavesi B.Archimedes Mission Aspects[A].IEE Colloquium on Highly Elliptical Orbit Satellite Systems[C].London,UK.24 May 1989,11/1-11/6.
[114]杨维廉.临界倾角与冻结轨道[J].宇航学报.1993.7.(3):1-9.
[115]ftp://ftp.igscb.jpl.nasa.gov.
[116]张艳.基于星间观测的星座自主导航方法研究[D].国防科技大学博士学位论文,2005.9.
[117]赵黎平,周凤岐,周军.实现轨道偏心率协调控制的卫星轨道维持方法[J].西北工业大学学报.Feb.2002.20(1):125-127.
[118]项军华,张育林.卫星姿态控制稳定度对星座构形稳定性的影响研究[J].航天控制,Jun.2007,25(3):43-47.
[119]杨嘉墀.航天器轨道动力学与控制(上)[M].北京:宇航出版社,1995.12.
[120]Wickert DP,Shaw GB,Hastings D.Impact of a Distributed Architecture for Space-Based Radar[J].Journal of Spacecraft and Rockets,Sep.-Oct.1998,35(5):703-713.
[121]Tollefson MV,Preiss BK.Space Based Radar Constellation Optimization[A].Proceedings of Aerospace Conference 1998[C],March 1998.3:379-388.
[122]任萱.人造地球卫星轨道动力学[M].长沙:国防科技大学出版社,1988.
[123]范丽,张育林.同构双基地雷达星座优化设计[J].系统工程与电子技术,Nov.2005. 27(1):1883-1888.
[124]Cornara S,Beech TW,Bello-Mora Met al.Satellite Constellation Launch,Deployment,Replacement and End-Of-Life Strategies[A].SSC99-X-1,13th Annual AIAA/USU Conference on Small Satellite[C],Logan,Utah,23-26 Aug.1999.
[125]Slattery R,Kovach Karl.New and Improved GPS Satellite Constellation Availability Model[A],ION GPS'99[C],Nashville,TN,14-17 Sept.1999.2103-2112
[126]Garrison TP,Ince M,Pizzicaroli J et al.Systems Engineering Trades for the IRIDIUM Constellation[J].ournal of Spacecraft and Rockets,1997.34(5):675-680.
[127]Xie M,Dai Y S,Poh K L.Computing System Reliability:Models and Analysis[M].New York:Kluwer Academic/Plenum Publishers,Apr.2004.
[128]郭齐胜,郅志刚,杨瑞平等.装备效能评估概论[M].北京:国防工业出版社,2005.8.
[129]Brian E.Operations Planning and Formation Flying:Analyzing Resource Usage in Formation Assembly[A].Proceedings of the 13th Annual AIAA/USU Conference on Small Satellites[C].Logan,Utah,23-26 Aug.1999.1-11.
[130]王永澄,付锋,陈晓凤.圆轨道同步卫星在区域导航系统中的应用[J].南京航空航天大学学报,2002,34(4):359-363.
[131]王莉.区域导航卫星系统的星座设计与比较[J].飞行器测控学报,1999.18(4)1-8.
[132]荆武兴.高长生.亚太区域导航八星星座分析[J].航天控制,Jul.2005,23(6):4-8.
[133]胡松杰.卫星星座的动力学研究[D].南京:南京大学博士学位论文,2003.12.
[134]申培萍.全局优化方法[M].北京:科学出版社.2006.3.
[135]徐玖平,李军.多目标决策的理论与方法[M].北京:清华大学出版社.2005.3.
[136]玄光男,程润伟著;于歆杰,周根贵译.遗传算法与工程优化[M].北京:清华大学出版社.2004.1.
[137]郦苏丹,朱江,李广侠.采用遗传算法的中轨区域通信星座优化设计[J].系统仿真学报,Jun.2005.17(6):1366-1369.
[138]赵勇,颜力,陈小前,王振国.基于MDO方法的月球探测卫星总体设计[J].上海航天,2006.(2):37-41.
[139]徐亚栋,钱林方.复合材料身管热-结构分析与优化[J].弹道学报,Jun.2006.18(2):31-35.
[140]iSIGHT Reference Guide.
[141]Back T.Selective Pressure in Evolutionary Algorithms:a Characterization of Selection Mechanisms[A].Proceedings of the First IEEE Conference on Evolutionary Computation(ICEC94)[C],Orlando,Dlorida,1994.57-62.
[142]Goldberg D,Korb B,Deb K.Messy Genetic Algorithms:Motivation,Analysis,and First Results[J].Complex System,1989.3:493-530.
[143]杨嘉墀.航天器轨道动力学与控制(下)[M].北京:宇航出版社,2001.12.
[144]毛悦,孙付平.利用Walker星座实现全球导航卫星星座设计[J].测绘科学技术学报,Apr.2006,23(2):153-156.
[145]http://www.calt.com/.
[146]范丽,张育林.Walker星座星间链路构建准则及优化设计研究[J].飞行力学,Jun.2007,25(3):93-96.
[147]王振永,王平,顾学迈等.卫星网络中永久星间链路的设计方法研究[J].通信学报,Aug. ?2006, 27(8): 129-33.
[148] Salzwedel KH, Freund H, Schorcht U. Examination of the Circular Polar Satellite Constellation for the Use of Inter-Satellite Links[A], Personal Wireless Communication of 1997 IEEE International Conference[C], Mumbai, India, Dec. 1997.283-287.
[149] Fonseca CM, Fleming PJ. Genetic Algorithms for Multiobjective Optimization: Formulation,Discussion and Generalization[A]. Proceedings of the 5th International Conference on Genetic Algorithms[C], Sam Mateo, CA, Jul. 1993. 416-423.
[150] Horn J, Nafpliotis N. Multiobjective Optimization Using the Niched Pareto Genetic Algorithm[R]. IlliGAL Report 93005, Illinois Genetic Algorithms Laboratory, University of Illinois, Urbana, Champaign, Jul. 1993.
[151] Srinivas N, Deb K. Multiobjective Optimization Using Nondominated Sorting in Genetic Algorithms[J]. Journal of Evolutionary Computation, 1995. 2(3):221-248.
[152] Zitzler E, Thiele L. Multiobjective Evolutionary Algorithm: A Comparative Case Study and the Strength Pareto Approach[J]. IEEE Transactions on Evolutionary Computation, 1999.3(4):257-271.
[153] Zitzler E, Laumanns M, Thiele L. SPEA2: Improving the Strength Pareto Evolutionary Algorithm[R]. TIK-Report 103, Computer Engineering and Networks Laboratory(TIK),Swiss Federal Institute of Technology(ETH), Zurich, Switzerland, May 2001.
[154] Watanabe S, Hiroyasu T, Miki M. Neighborhood Cultivation Genetic Algorithm for Multi-Objective Optimization Problems[A].Proceedings of 4th Asia-Pacific Conference on Simulated Evolution and Learning(SEAL'02)[C], Orchid Country Club, Singapore, Nov.2002.1:198-202.
[155] Deb K, Agrawal S, Pratap A et al. A Fast Elitist Non-Dominated Sorting Genetic Algorithm for Multi-Objective Optimization: NSGA-II[R]. Kanpur Genetic Algorithms Laboratory Report No. 200001. Kanpur Genetic Algorithms Laboratory, Indian Institute of Technology Kanpur, Kanpur India, 2000.
[156] Deb K, Pratap A, Agarwal S et al. A Fast and Elitist Multiobjective Genetic Algorithm:NSGA-II[J]. IEEE Transactions on Evolutionary Computation, Apr. 2002, 6(2):182-197.
[157] Walker JG. Satellite Constellation[J]. Journal of the British Interplanetary Society, 1984,37:559-571.
[158] Adams RJ, Buffmgton JM, Banda SS. Robust, Nonlinear, High Angle-of-Attack Control Design for a Supermaneuverable Vechicle[R]. NTIS No: N9425108/9/HDM.
[159] Adams WS, Rider L. Circular Polar Constellations Providing Continuous Single or Multiple Coverage above a Specified Latitude[J] Journal of Astronautical Science, 1987.35(3):155-192.
[160] Salgado G, Abbondanza S, Blondel R et al. Constellation Availability Concepts for Galileo[A]. ION NTM 2001[C], Long Beach, CA, 22-24 Jan. 2001. 778-786.