期刊文献+

实现PBN技术的陆基DME台选择算法 被引量:4

DME selection algorithm for implementation of PBN technology
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摘要 航路飞行阶段的导航台选择是区域导航(area navigation,RNAV)运行的主要环节。在RNAV选台过程中通常会遇到换台频繁或台站跳变问题。根据测距机(distance measure equipment,DME)/DME导航方式提出了实际导航性能(actual navigation performance,ANP)的计算方法,并通过设定ANP阈值结合最小ANP值的方法设计航路飞行阶段DME台站选择算法。对京沪航线及其周围的DME台站数据进行了仿真实验,结果表明,该选台算法在满足导航精度要求的情况下有效避免了换台频繁和台站跳变问题。 The navigation station selection is a major aspect of the area navigation(RNAV) in en-route phase of flight. The common problems are the frequent station switching and the navigation station hopping in RNAV station selection. Actual navigation performance(ANP) calculation is presented by the distance measure equipment(DME)/DME navigation way, and a DME station selection algorithm is designed by setting the ANPthreshold combining with the least ANP in en-route phase of flight. Some simulation experiments are performed using the data about Beijing Shanghai route and its surrounding DME stations. The results show that the station selection algorithm meets the requirements of navigation accuracy while effectively avoiding the frequent station switching and the navigation station hopping.
出处 《系统工程与电子技术》 EI CSCD 北大核心 2013年第10期2170-2175,共6页 Systems Engineering and Electronics
基金 中央高校基本科研业务费中国民航大学专项项目(ZXH2012H002)资助课题
关键词 导航台选择 基于性能导航 区域导航 测距机 实际导航性能 station selection performance based navigation area navigation(RNAV) distance measure equipment(DME) actual navigation performance (ANP)
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参考文献14

  • 1ICAO Doe 9613. Performance based navigation(PBN) manual[S]. Canada: International Civil Aviation Organization, 2008.
  • 2ICAO Doc 8168. Aircraft operations volume Ⅱ construction of visual and instrument flight procedure[S]. Canada: lnternation al Civil Aviation Organization, 2006.
  • 3ICAO Annex 10. Aeronautical telecommunications volume I ra dio navigation aids[S]. Canada: International Civil Aviation Or ganization, 2006.
  • 4石宝峰,程朋,程农.区域导航进近阶段导航台选择模型与仿真[J].系统仿真学报,2011,23(10):2039-2045. 被引量:6
  • 5曹刚,辛格.基于性能评估的INS/RADIO组合导航系统研究[J].科技创新导报,2011,8(31):13-15. 被引量:2
  • 6中国民用航空局.基于性能的导航实施路线图[EB/OL].[2009-10-27].ht-tp://www.caac.gov.cn/dev/fbs/XJSYY/200910/P020091118303-195333915.pdf.
  • 7中国民用航空局.RNAV5运行批准指南[EB/OL].[2008-02-22].http://sqgk.caac. gov. cn/OOOO14170/200802/t20080222_8193, htm.
  • 8Baritone C G. A terrestrial positioning and timing system (TPTS) [C]//Proc. of the Position Location and Navigation Symposium, 2012:1175 - 1182.
  • 9Herndon A A, Cramer M, Nicholson T, et al. Analysis of ad vanced flight management systems(FMS), flight management corn puter(FMC) field observations trials: area navigation(RNAV) holding patterns[C]//Proc, of the 30th Digital Avionics Systems Conference, 2011:4A1 - 1 - 4A1 - 17.
  • 10Euiho K. Investigation of APNT optimized DME/DME network using current state-of-the-art DMEs [C] // Proc. of the Position Location and Navigation Symposium, 2012:146 - 157.

二级参考文献21

  • 1金辽.论全向信标和测距仪的信号覆盖[J].航空电子技术,2003(z1):49-53. 被引量:3
  • 2周其焕.利用飞行管理系统实现组合导航[J].导航,1990(4):19-30. 被引量:1
  • 3王胜标,王俊璞,倪静静,田蔚风,金志华.GPS/INS组合导航算法性能评估平台[J].中国惯性技术学报,2007,15(2):181-184. 被引量:8
  • 4钦庆生.飞行管理计算机系统[M].北京:国防工业出版社,1991.
  • 5ICAO, Performance based navigation Manual [ R ]. Montr6al : International Civil Aviation organization, 2008.
  • 6Roxancb Chamlou, TIS-B : Calculation of navigation accuracy category for position and velocity parameters [C ]. New York: IEEE proceedings, 2004.
  • 7BCAG Engineering, RNP capability of FMC equipped 737 [ R ]. Seattle: Boeing Company, 2003.
  • 8RTCA DO236, Minimum aviation system performance standards: Required navigation performance for area navigation[ R]. Washington D. C. : RTCA Inc. , 2003.
  • 9Jennifer D G, GPS/INS Generalized evaluation tool for the design and testing of integrated navigation systems [ D]. USA: Stanford University, 2003.
  • 10T. Walter, J. Blanch, et al. Evaluation of Signal in Space Error Bounds to Support Aviation Integrity [ C ]. Savannah GA: ION GNSS, 2009.

共引文献27

同被引文献28

  • 1隋东,隋东,王炜,左凌.基于DME/DME的区域导航航路导航性能评估方法[J].交通运输系统工程与信息,2006,6(4):24-28. 被引量:8
  • 2黄卫芳.浅谈基于性能导航(PBN)[J].空中交通管理,2007(7):10-16. 被引量:12
  • 3Yin Y, Liu B, Su D. Research on formal verification tech- nique for aircraft safety-critical software[ J]. Journal of Computers,2010,5(8) : 1152-1159.
  • 4Esposito C, Barbosa R, Silva N. Safety-Critical Standards for Verification and Validation[ C ]//Proceedings of Inno- vative Technologies for Dependable OTS- Based Critical Systems. Milan : Springer,2013:41-53.
  • 5Chen Z, Gu Y, Huang Z Q, et al. Model checking aircraft controller software : a case study [ J ]. Software : Practice and Experience ,2013,44( 8 ) :2242.
  • 6Panesar-Walawege R K, Sahetzadeh M, Briand L. A mod- el-driven engineering approach to support the verification of compliance to safety standards [ C ]//Proceedings of 22th Software Reliability Engineering. [ S. l. ] : IEEE, 2011:30-39.
  • 7RTCA DO- 178B/ED- 12B, Software Considerations in Airborne Systems and Equipment Certification [ S ].
  • 8GB/T28441-2012,车载导航电子地图数据质量规范[S].
  • 9RTCA DO 201A, Standards for Aeronautical Information [S].
  • 10RTCA DO 200A, Standards for Processing Aeronautical Data[ S].

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