星群协同阵列传输容量

肖振宇; 李瑶; 白文杰; 白琳

doi:10.13700/j.bh.1001-5965.2014.0681

星群协同阵列传输容量

doi: 10.13700/j.bh.1001-5965.2014.0681

肖振宇¹,
李瑶²,
白文杰¹,
白琳^1, ,

1.
北京航空航天大学电子信息工程学院, 北京 100191
2. 北京航空航天大学高等工程学院, 北京 100191

基金项目: 国家自然科学基金(61201189,91338106,61231011,61231013); 中央高校基本科研业务费专项资金(YWF-14-DZXY-007,YWF-14-RSC-006,YWF-14-DZXY-020)

详细信息

作者简介:
肖振宇(1983—),男,湖北天门人,讲师,xiaozy06@gmail.com

通讯作者:
白琳(1982—),男,北京人,副教授,L.Bai@buaa.edu.cn,主要研究方向为空天通信网络及地面无线通信.

中图分类号: V443⁺.1;TN927⁺.2;TB553
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- 被引次数: 0
出版历程
- 收稿日期: 2014-11-04
- 网络出版日期: 2015-09-20

Channel capacity of cooperative grouped satellites with array based transmission

XIAO Zhenyu¹,
LI Yao²,
BAI Wenjie¹,
BAI Lin^{1
, ,}

1.
School of Electronic and Information Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100191, China
2. School of Advanced Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100191, China

摘要

摘要: 为进一步提升星群协同的系统容量,考虑在卫星星群上配置阵列天线的传输模式.分析了最大化容量时下行链路的信道条件,给出了系统容量最大化的实现方式,探索了系统参数对信道容量的影响,发现信道容量随地面天线间距成周期性变化,其周期与卫星数目成反比、与地面天线阵列相对于东西方向的夹角的余弦成反比、与相邻卫星之间的角间距成反比.在多卫星多天线环境下,发现信道容量曲线的包络同样随地面天线间距成周期性变化,提出并通过仿真验证了多卫星多天线环境下减小地面天线间距和降低测控精确度要求的地面天线排布方案.
- 阵列天线 /
- 星群协同 /
- 信道容量 /
- 多入多出 /
- 卫星信道模型
Abstract: In order to improve the system capacity of cooperative grouped satellites, we considered the transmission mode of equipping the satellites with antenna arrays. Channel condition of downlink with maximum channel capacity was analyzed. Implementation approaches to the maximum channel capacity were put forward. Influences of system parameters to the channel capacity were researched. The results show that the channel capacity changes with the ground antenna distance periodically. The changing cycle of the channel capacity curve is in inverse proportion to the number of satellites (sat-number), to the cosine value of the angle between the ground array and an east-west line and to the angular distance between satellites (sat-angular-distance). The envelope of the channel capacity curve changes with the ground antenna distance periodically as well in a multi-satellites multi-antennas environment. An arrangement strategy of ground antennas in a multi-satellites multi-antennas environment was proposed to decrease the ground antenna distance and to lower the requirement of the ground array measurement accuracy as well, which was verified by the simulation results.
- antenna arrays /
- cooperative grouped satellites /
- channel capacity /
- multiple-input multiple-output /
- satellite channel model

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参考文献(18)

[1]	Alagoz F,Gur G.Energy efficiency and satellite networking:A holistic overview[J].Proceedings of the IEEE,2011,99(11):1954-1979.
[2]	林来兴,张小琳.星群、星座与编队飞行的概念辨析[J].航天器工程,2012,21(5):97-102.Lin L X,Zhang X L.Discussion on conception of cluster,constellation and formation flying[J].Spacecraft Engineering,2012,21(5):97-102(in Chinese).
[3]	Massonet D.Capabilities and limitations of the interferometric cartwheel[J].IEEE Transactions on Geoscience and Remote Sensing,2001,39(3):506-520.
[4]	Krieger G,Moreira A,Fiedler H,et al.TanDEM-X:A satellite formation for high-resolution SAR interferometry[J].IEEE Transactions on Geoscience and Remote Sensing,2007,45(11):3317-3339.
[5]	Moccia A.A bistatic SAR for earth observation[J].The International Society for Optical Engineering,2000,4173:1-9.
[6]	D'Errico M,Moccia A.The BISSAT mission:A bistatic SAR operating information with COSMO/SkyMed X-band radar[C]//Aerospace Conference Proceedings.Piscataway,NJ:IEEE Press,2002:2-809-2-818.
[7]	Martin M,Klupar P,Kilberg S,et al.TechSat21 and revolutionizing space missions using microsatellites[C]//15th American Institute of Aeronautics and Astronautics Conference on Small Satellites.Reston:AIAA,2001:1-10.
[8]	Lee P F,Girard R,James K.The RADARSAT-2&3 topographic mission:An overview[C]//Geoscience and Remote Sensing Symposium,2002.IGARSS '02.2002 IEEE International.Piscataway NJ:IEEE Press,2002:3-1477-3-1479.
[9]	杨海平,胡向晖,李毅,等.卫星通信系列讲座之十三先进极高频(AEHF)卫星[J].数字通信世界,2008(6):84-87.Yang H P,Hu X H,Li Y,et al.The advanced extremely high frequency(AEHF)satellite[J].Digital Communication World,2008(6):84-87(in Chinese).
[10]	杭观荣,康小录.美国AEHF军事通信卫星推进系统及其在首发星上的应用[J].火箭推进,2011,37(6):1-8.Hang G R,Kang X L.Propulsion system of USA AEHF military communication satellite and its application on AEHF-1 satellite[J].Journal of Rocket Propulsion,2011,37(6):1-8(in Chinese).
[11]	吴学智,武兵,何如龙,等.外军新一代卫星通信系统及关键技术研究[J].通信技术,2012(9):7-9.Wu X Z,Wu B,He R L,et al.Research of new generation of satellite communication system in foreign military and its key technology[J].Communication Technology,2012(9):7-9(in Chinese).
[12]	Steyskal H,Schindler J K,Franchi P,et al.Pattern synthesis for techSat21-A distributed space-based radar system[J].IEEE Antennas and Propagation Magazine,2003,45(4):19-25.
[13]	冯少栋,张卫峰,张晓静,等.美军下一代转型卫星运控系统设计[J].数字通信世界,2009(5):59-63.Feng S D,Zhang W F,Zhang X J,et al.Design of next generation TSAT operating system of U.S.army[J].Digital Communication World,2009(5):59-63(in Chinese).
[14]	Maral G,Bousquet M.Satellite communications systems:Systems,techniques and technology[M].2nd ed.Chichester:Wiley,1993:206-216.
[15]	Schwarz R T,Knopp A,Lankl B,et al.Optimum-capacity MIMO satellite link for fixed and mobile services[C]//International ITG Workshop on Smart Antennas (WSA 2008).Piscataway,NJ:IEEE Press,2008:209-216.
[16]	Telatar E.Capacity of multi-antenna Gaussian channels[J].European Transactions on Telecommunications,1999,10(6):585-595.
[17]	周杰,陈靖峰,邱琳,等.三维空间MIMO信道接收天线阵列互耦效应及系统容量分析[J].通信学报,2012,33(6):1-10.Zhou J,Chen J F,Qiu L,et al.Effect of mutual coupling and antenna correlation on MIMO system in three-dimensional spatial channel models[J].Journal on Communications,2012,33(6):1-10(in Chinese).
[18]	Schwarz R T,Knopp A,Lankl B,et al.Optimum-capacity MIMO satellite broadcast system:Conceptual design for LOS channels[C]//4th Advanced Satellite Mobile Systems.Piscateway,NJ:IEEE Press,2008:60-65.