期刊文献+

三种卫星故障检测策略的对比研究与仿真 被引量:6

Comparison and Simulation of Three Satellites' Failure Detection Methods
下载PDF
导出
摘要 故障检测是保证导航系统完好性的重要途径。针对接收机自主完好性监测算法RAIM需要至少5颗可见星时才能进行故障检测的问题,在惯性/卫星组合导航系统的框架下,通过构建能反映卫星故障特征的检验统计量,并根据检验统计量的分布确定相应的检测门限,提出了解分离和残差外推两种卫星故障检测方案。仿真结果表明:解分离算法能在存在RAIM漏洞时检测故障且易于进行系统重构,但其故障检测效率不高;残差外推法适用于检测慢变故障。仿真结果表明,改进方法故障检测效率有较大提高,甚至在只有三颗可见星时仍能较快地检测出慢变故障。 Failure detection is an important way to guarantee the integrity requirement of navigation system.In order to deal with the problem of RAIM's requirement of at least five visible satellites to complete failure detection,in the frame of inertial/satellite integrated navigation system,by establishing detecting statistics that can reflect the satellites' failure and calculating the corresponding detection thresholds,two schemes of solution separation and residue extrapolation were proposed to detect the satellites' failures.The analysis and simulation show that the solution separation method can successfully detect satellites' failures even under RAIM hole condition,and the system can easily complete configuration with this scheme,but the failure detecting efficiency is not very high; residue extrapolation method takes the advantage of detection slowly growing failure,and its failure detection efficiency is greatly improved,and it can quickly detect slowly growing failure even there being only three visible satellites.
出处 《计算机仿真》 CSCD 北大核心 2013年第9期51-55,共5页 Computer Simulation
基金 陕西省自然科学基金(2012JM8035) 空军工程大学航空航天工程学院科研创新基金(XS1101021)
关键词 完好性 故障检测 接收机自主完好性监测 解分离 残差外推 Integrity Failure detection RAIM Solution separation Residue extrapolation
  • 相关文献

参考文献7

二级参考文献31

  • 1周坤芳,孔键,周湘蓉.紧耦合GPS/INS组合导航能力的分析[J].中国惯性技术学报,2005,13(6):50-53. 被引量:8
  • 2高化猛,赵新国,李智.飞行器INS与GPS组合导航系统卡尔曼滤波[J].装备指挥技术学院学报,2007,18(1):59-62. 被引量:6
  • 3陈偲,王可东.惯性导航与卫星导航紧耦合技术发展现状[J].全球定位系统,2007,32(3):21-26. 被引量:18
  • 4Umar lqbal Bhatti, An Improved Sensor Level Integrity Algorithm for GPS/INS Integrated System[C]. Proceedings of ION GNSS 19^th International Technical Meeting, 2006.
  • 5Hong, S, Lee et al. Observability of Error States in GPS/INS Integration[J]. IEEE Transactions on Vehicular Technology, 2005, 54(2).
  • 6John H. Wall and David M. Bevly. Characterization of Inertial Sensor Measurements for Navigation Performance Analysis[C]. Proceedings of ION GNSS 19^th International Technical Meeting, 2006.
  • 7Carlson,N.A. Federated Kalman Filter Simulation Results[J], Navigation, 1994, 41 (3): 297- 321.
  • 8Kondo S, Kubo N, Yasuda A. Evaluation of the pseudo range performance by using software GPS receiver[J]. Journal of Global Positioning System, 2005(4): 215-222.
  • 9Alban S. Performance analysis and architectures for INS-aided GPS tracking loops[C]//ION National Technical Meeting, Jan. 2003: 22-24.
  • 10Chiou T, Alban S, Atwaer S. Performance analysis and experimental validation of a Doppler-aided GPS/INS receiver for JPALS applications [C]//Proceedings of ION GNSS 17th International technical meeting of the satellite division. Long Beach, 21-24 September, 2004: 1609-1618.

共引文献44

同被引文献40

引证文献6

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