期刊文献+

多任务卫星簇适应性轨道设计

Optimal Design for Multi-Task Satellite Cluster Adaptive Orbit
下载PDF
导出
摘要 卫星簇是介于卫星编队和卫星星座之间的一种新的空间组网卫星构型。通过多颗卫星联合工作,组网卫星簇能够提高对指定区域的覆盖时间,扩展对地面的观测范围。针对多任务卫星簇,提出了一种满足多种载荷任务约束的适应性轨道方案。将多任务卫星簇分为侦察卫星簇和长时间连续覆盖卫星簇两部分:侦察卫星簇在实现全球快速侦察的同时,能够弥补对热点区域的连续覆盖时间;连续覆盖部分卫星簇在实现区域长时间连续覆盖的同时,可以拓展对地球的侦察区域。仿真结果表面,若载荷天线波束为60°,有效作用距离为1 200 km,那么只需要6颗卫星就可以每天对全球进行1次侦察,并且对热点区域的连续覆盖时间超过20 min。 Satellite cluster is a new kind of space configuration different from satellite formation and satellite con-stellation. With multi-satellites working together, satellites can improve the covering time span for the assigned re-gion and broaden the observation area on the earth. For the multi-task satellite cluster, an adaptive orbit scheme that satisfied various payload constraints was proposed. The multi-task satellite cluster was divided into two parts:the reconnaissance cluster and the long-time covering cluster. The reconnaissance cluster can observe the earth quickly while increasing the covering time for the assigned region. The covering cluster can observe the assigned re-gion with the longest time while enlarging the covered area on the earth;this was beneficial to the global reconnais-sance. Simulation results and their analysis manifested preliminarily that, when the antenna beam was 60°; and the effective distance was 1 200 km, only six satellites are necessary for observing the earth each day and the covering time for the assigned region was more than 20 minutes.
出处 《西北工业大学学报》 EI CAS CSCD 北大核心 2014年第5期834-839,共6页 Journal of Northwestern Polytechnical University
基金 国家自然科学基金(61304238) 国家高技术研究发展计划(2012AA120602) 中央高校基本科研业务费(3102014JCQ01004)资助
关键词 区域覆盖 全球侦察 轨道 多任务 优化设计 卫星簇 antennas, computer simulation, constrained optimization, design, MATLAB, multitasking, orbits,radar, satellite communication systems earth reconnaissance, region covering
  • 相关文献

参考文献10

  • 1Leonel M, Pini G. Cluster Flight Algorithms for Disaggregated Satellites [ J ]. Journal of Guidance, Control, and Dynamics, 2013, 36(1) : 124-135.
  • 2Dario Izzo. Autonomous and Distributed Motion Planning for Satellite Swarm [ J ]. Journal of Guidance, Control, and Dynamics, 2007, 30(2): 449-459.
  • 3Sharon D V, Brett N. Designing a Constrained Optimal Orbit for Earth Observation Satellites Based on User Requirements[ C ]// AIAA/AAS Astrodynamics Specialist Conference, Toronto, Ontario Canada, 2010.
  • 4David R, Lawrence J. Continuous Zonal Coverage[ C ]//AIAA Mechanics and Control of Flight Conference, Anaheim, Califor- nia, 1974.
  • 5王启宇,袁建平,朱战霞.对地观测小卫星星座设计及区域覆盖性能分析[J].西北工业大学学报,2006,24(4):427-430. 被引量:7
  • 6Franqois D. Coverage Optimization of Elliptical Satellite Constellations with Extended Satellite Triplet Method [ C ]//54th Interna- tional Astronautical Congress of the International Astronautical Federation, Bremen, Germany, 2003.
  • 7Jochim E F M, Pietrass A E, Kirschner M. The Local Coverage Diagram[ C ] ffAIAA/AAS Astrodynamics Specialist Conference and Exhibit, Honolulu, Hawaii, 2008.
  • 8王海丽,陈磊,任萱.三星时差定位卫星簇的分析与设计[J].国防科技大学学报,2001,23(4):6-9. 被引量:13
  • 9Bong Wie. Spacecraft Vehicle Dynamics and Control, Second Edition[ M ]. AIAA Education Series Reston, VA, USA, 2008.
  • 10郑永安,马瑞卿.双自由度步进电动机在卫星天线控制中的应用[J].微电机,2005,38(6):50-53. 被引量:1

二级参考文献15

  • 1James Andrus and Ed Korzeniowski. Modular Antenna Pointing System for the Explorer Platform Satellite[J]. Honeywell Inc., Satellite Systems Operation,Presented at the 26th Aerospace Mechanisms Symposium,May, 1992.
  • 2Z. Y. Yi and P. T. Mathiopoulos. Antenna pointing in LEO/MEO satellite systems for mobile applications[J]. 5th European Conference in Satellite Communications ,November, 1999.
  • 3Ohishi K. , Someno T., Advanced motion control in redundant motion systems [J]. Advanced Motion Control, 5th International Workshop on AMC,Coimbra,Jun, 1998.
  • 4Mizutami K, Hayashi S, Matsui N. Modeling and Control of Hybrid Setpping Motors[J]. Proc of 16th IEEE Industry Application Society Conference,San Antonio ,TX, USA, 1993 : 289- 294.
  • 5Szasz C,Marschalko R,Trifa V,et al. Data Acquisition and Signal Processing in Vector Control of PWM Hybrid Stepping Motor EJ-]. Proc of the 6th IEE International Conference on Optimization of Electrical and Electronic Equipments, Cluj, Romania, 1998:447-450.
  • 6Chen WD, Yung KL, Cheng KW. Enhancing Low-speed Performance of Hybrid Stepping Motor Servo by Ripple Canceling Technique [J]. Proc of IEEE Iternational Conference on Electric Machines and Drives, Hong Kong, 1997 : 147- 149.
  • 7Freitas, M. A. A. Andrade, D. A. Borges, T. T.Azevedo, H. R. Driving the step motor with controlled phase currents[J]. Procedings of the IEE International Conference on Power Electronics,Drives and Energy Systems for Industrial Growth,PEDES 1998,2 : 493- 498.
  • 8Fan, Xiao - ming; Zhang, Li ;Wang, Guo - dong ; Liu,Xiang - hua ;Han. An - rong Control system of two phase hybrid step motor based on the torque star vector mode [J]. Dongbei Daxue Xuebao/Journal of Northeastern University, 2000,21 (1) : 101- 103.
  • 9Bottkol M S, DiDomenico P B. A Phase-Based Approach to the Satellite Revisit Problem. AAS 91-900:865-884
  • 10Evans M J. Optimization of Satellite Constellation for Partial Coverage. Colorado: University of Colorado, 1999

共引文献18

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部