期刊文献+

基于未确知数的PBN导航下的空中立交桥模型优化 被引量:3

Optimization of aerial overpass model based on PBN navigation of unascertained number
原文传递
导出
摘要 通过建立新型空中立交桥对航路交叉点进行优化,达到航路扩容的目的,使得交叉点的容量尽可能地与航路容量接轨,以解决交叉点对航路容量的限制问题。基于航空器在飞行中有很多无法确定的参数这一特征,将未确知数理论引入交叉点容量计算,并建立了空中立交桥的未确知数模型,得到了航空器在新型立交桥附近的各种可能区间以及其可信度水平,弥补了传统确定性模型的不足。通过在交叉点附近实行RNAV1导航规范,提高交叉点附近的导航精度。计算结果表明,在3种不同系数下,优化后的空中立交桥比优化前的容量分别增加了75.61%,74.39%和75.95%。 By establishing a new type of aerial overpass to optimize the intersection of the route,realize the purpose of extending the route,so that the capacity of the intersection is as close as possible to the capacity of the route,and the limitation of the route capacity at the intersection is solved.Based on the fact that the aircraft has many undetermined parameters in flight,the unascertained number theory is introduced into the intersection capacity calculation,and the unascertained number model of the aerial overpass is established.Various possibilities of the aircraft near the new overpass are obtained.The interval and its level of credibility compensate for the shortcomings of the traditional deterministic model.By implementing the RNAV1 navigation specification near the intersection,the navigation accuracy near the intersection is improved.Calculation results show that the optimized aerial overpass increases by 75.61%,74.39%and 75.95%respectively with the use of the three different coefficients.
作者 戴福青 吴佳轩 DAI Fu-qing;WU Jia-xuan(College of Air Traffic Management,Civil Aviation University of China,Tianjin 300300,China)
出处 《飞行力学》 CSCD 北大核心 2019年第5期68-71,75,共5页 Flight Dynamics
基金 国家自然科学基金资助(61571441) 国家重点研发计划资助项目(2016YFB0502405)
关键词 未确知数 基于性能导航 交叉点 空中立交桥 unascertained number PBN intersection aerial overpass
  • 相关文献

参考文献6

二级参考文献36

  • 1王永泉,陈花玲,毛文雄.基于跟驰理论的道路交通噪声预测模型研究[J].系统仿真学报,2004,16(11):2413-2416. 被引量:8
  • 2杨军利,方群,向小军.终端区飞机排序的规划模型和算法研究[J].飞行力学,2005,23(2):77-80. 被引量:7
  • 3岳常安,吴和琴,徐东明.未确知有理数的定义、运算及在建筑工程中的应用[J].数学的实践与认识,1995,25(4):14-19. 被引量:25
  • 4许时芬,谷风.不完整信息的数学处理方法[J].自然杂志,1996,18(6):327-331. 被引量:8
  • 5Performance-based navigation (PBN) manual. 3rd ed. DOC 9613-AN/937. Montreal: International Civil Aviation Organization, 2008.
  • 6Anderson M R. Flight technical error model for nonstationary random turbulence. AIAA-2001-4265, 2001.
  • 7Levy B S, Som P, Greenhaw R. Analysis of flight technical error on straight, final approach segments. 59th Annual Meeting Proceedings of ION. 2003; 456-467.
  • 8Hall T, Soares M S. Analysis of localizer and glide slope flight technical error. IEEE/AIAA 27th Digital Avionics Systems Conference. 2008; 2.D.2-1-2.D.2-9.
  • 9Williams D M, Consiglio M C, Murdoch J L, et al. Flight technical error analysis of the SATS higher volume operations simulation and flight experiments. 24th Digital Avionics Systems Conference. 2005; 13.B.l-l-13.B.l-12.
  • 10Doyle J C, Stein G. Multivariable feedback design: concepts for a classical/modern synthesis. [EEE Transactions on Automatic Control 1981 ; 26(1 ): 4-16.

共引文献55

同被引文献20

引证文献3

二级引证文献1

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