期刊文献+

基于类GPS技术的编队卫星相对参数测量研究 被引量:2

Measurement of Relative Parameters of Formation Fight Satellites Based on Quasi-GPS Technology
下载PDF
导出
摘要 针对编队飞行小卫星间相对位置和相对姿态的测量,提出利用类GPS技术实现编队卫星间的自主测量,建立相应的测量模型来获得与相对位置和相对姿态相关的观测量。利用C-W方程和姿态运动学方程建立相应的状态方程,通过扩展卡尔曼滤波实现对编队卫星间相对参数的实时估计。MATLAB仿真结果表明,此方法能够获得很高的测量精度。 Quasi-GPS(Global Positioning System) technology is used to achieve autonomous measurement of formation flight satellites and to establish a measurement model to obtain observables of relative position and attitude.C-W equations and attitude kinematics equations are used to establish state equations for real-time estimation of the relative parameters of formation flight satellites with an extended Kalman filter.As shown by MATLAB simulation results,a high measurement accuracy is got.
出处 《飞行器测控学报》 2012年第3期85-89,共5页 Journal of Spacecraft TT&C Technology
基金 国家自然科学基金(60974107) 教育部博士点基金(20070287007)
关键词 编队卫星 类GPS 相对位置 相对姿态 位姿测量 formation flight satellites quasi-GPS relative position relative attitude measurement of position and attitude
  • 相关文献

参考文献6

  • 1钱萍,王惠南.基于三目视觉测量的航天器交会对接相对位姿确定算法[J].宇航学报,2010,31(6):1575-1581. 被引量:13
  • 2Chung S J, Ahsun U, Slotine J J E. Application of Synchro- nization to Formation Flying Spacecraft: Lagrangian Ap- proaeh[J]. Journal of Guidance, Control, and Dynamics, 2009,32(2) : 512 - 526.
  • 3Corazzini Noel Tobey. Onboard Pseudolite Augmentation for Spacecraft Formation Flying[D]. California: Stanford Uni- versity, 2000.
  • 4陈谷仓,王元钦,王天祥,陈宏.编队小卫星相对位置和相对姿态解算模型与精度分析[J].系统仿真学报,2005,17(11):2600-2603. 被引量:5
  • 5Junkins J L, Hughes D C, Wazni K P. Visiombased Naviga tion for Rendezvous, Docking, and Proximity Operations[J]. Advances in the Astronautieally Sciences, 1999, 101:203 22O.
  • 6王惠南.GPS导航原理与应用[M].北京:科学出版社,2008:197-203.

二级参考文献13

  • 1张庆君,胡修林,叶斌,钟山.基于双目视觉的航天器间相对位置和姿态的测量方法[J].宇航学报,2008,29(1):156-161. 被引量:44
  • 2曹喜滨,张世杰.航天器交会对接位姿视觉测量迭代算法[J].哈尔滨工业大学学报,2005,37(8):1123-1126. 被引量:27
  • 3HOCJ,MCDLAMROCHNH.Automatic spacecraft docking using computer vision-based guidance and control techniques[J].Journal of Guidance,Control,and Dynamics,1993,16(2):281-288.
  • 4PHILIPNK,ANANTHASAYANAMMR.Relative position and attitude estimation and control schemes for the final phase ot an autonomous docking mission of spacecraft[J].Acta Astronautica,2003,52:511-522.
  • 5马颂德 张正友.计算机视觉-计算理论与算法基础[M].北京:科学出版社,1997..
  • 6Sien ChongWu, DaKuang. Positioning With Autonomous Formation Flyer (AFF) on Space Technology 3[C]. IONGPS'99,Nashville,TN, 14-17 September, 1999.
  • 7H.Beyer. Geometric and Radiometric Analysis of a CCD-Camera Based Photogrammetric Close-Range System. PhD thesis[C]. ETH, Z Urich, 1992.
  • 8Sullivan W. Performance Analysis of an Integrated GPS/Inertial Attitude Determination System[Z]. US: MIT, 1994.
  • 9Shuster, M. D, Oh, S. D. Three-Axis Attitude Determination from Vector Observations[J]. Guidance and Control, 1981, 8:56-63.
  • 10Sunny Leung. High Precision Real-Time Navigation for Spacecraft Formation Flying[Z]. ION GPS 2003, Portland, Oregon, September 9-12, 2003.

共引文献22

同被引文献22

  • 1李晨光,韩潮.编队飞行卫星群相对轨道测量研究[J].北京航空航天大学学报,2005,31(6):614-617. 被引量:4
  • 2刘洋,易东云,王正明.编队卫星的状态测量方法综述及可行的高精度星间基线测量方案研究[J].航天控制,2006,24(3):65-69. 被引量:6
  • 3WU Yunhua, CAO Xibin, XING Yanjun, et al. Relative motion coupled control for formation flying spacecraft via convex optimization [ J ]. Aerospace Science and Technology, 2010,14: 415-428.
  • 4WU Yunhua, CAO Xibin, XING Yanjun, et al. Relative motion integrated coupled control for spacecraft formation via Gauss Pseudospectral method [ J ]. Transactions of the Japan Society for Aeronautical and Space Sciences, 2009, 52(177) : 125-134.
  • 5WU Baolin, WANG Danwei, ENG K P, et al. Nonlinear optimization of low-thrust trajectory for satellite formation: Legendre Pseudospectral approach : J ]. Journal of Guidance, Control, and Dynamics, 2009, 32 (4) :1371-1381.
  • 6WU Yunhua, GAO Yang, LIN Jiawei, et al. Low-cost, high-performance monocular vision system for air bearing table attitude determination [ J ]. Journal of Spacecraft and Rockets, 2014,51(1): 66-75.
  • 7CRASSIDIS J L, ALONSO R, JUNKINS J L. Optimal attitude and position determination from line-of-sight measurements [ J ]. The Journal of the Astronautical Sciences, 2000, 48(2/3) : 891-896.
  • 8CHENG Y, CRASSIDIS J L, MARKLEY F L. Attitude estimation for large field-of-view sensors [ J ]. Journal of the Astronautical Sciences, 2006, 54(3/4) : 433-448.
  • 9YANG Y, CAO X. Design and development of the small satellite attitude control system simulator [ C]//AIAA Modeling and Simulation Technologies Conference and Exhibit. Reston VA : AIAA, 2006:21-24.
  • 10HARALICK R M, JOO H, LEE C, et al. Pose estimation from corresponding point data [J]. IEEE Transactions on Systems, Man and Cybernetics, 1989, 19(6) : 1426-1446.

引证文献2

二级引证文献11

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