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Design of an aircraft landing system using dual-frequency GNSS.

机译:使用双频GNSS的飞机着陆系统的设计。

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摘要

There is a strong demand for new all-weather navigation aids to support aircraft precision approach and landing. The Federal Aviation Administration's Local Area Augmentation System (LAAS) is one such navigation aid that uses the Global Positioning System (GPS) to estimate aircraft location. LAAS is required to provide very high levels of accuracy, integrity, continuity, and availability, and the integrity requirement of one undetected navigation failure in a billion approaches has been a critical challenge in the design of this system. Tremendous efforts have developed methods to guarantee integrity for various potential anomalies that might threaten LAAS-aided landing. Currently, almost all these risks are mitigated by existing methods. One issue that remains is the risk due to ionosphere anomalies.; This dissertation introduces novel integrity algorithms for ionosphere anomalies that take advantage of GPS modernization---undergoing changes in the GPS system that enhance civil user capabilities. This modernization includes adding new GPS civil signals, and these signals make possible multiple-frequency techniques. This research focuses on two types of dual-frequency carrier-smoothing methods---Divergence-Free Smoothing and Ionosphere-Free Smoothing---and develops integrity algorithms for ionosphere anomalies using these methods.; Simulations show that the first algorithm, using Ionosphere-Free Smoothing, can achieve 96% to 99.9% availability at best over a broad region of the Conterminous United States (CONUS). This level of availability is unacceptably low for practical use. However, a benefit is that the resulting availability is not a function of the ionosphere condition. The second algorithm, based on Divergence-Free Smoothing, is shown by simulations to achieve more than 99.9% availability over more than 70% of CONUS under nominal ionosphere conditions. However, it has the potential to completely lose availability under severe ionosphere conditions. Taking advantage of these two algorithms, this research introduces a system architecture that implements both smoothing methods. The resulting system switches smoothing methods based upon the best estimate of the current ionosphere state obtained by an ionosphere monitor that is also designed as part of this research. This architecture can achieve more than 99.9% availability under nominal ionosphere conditions and more than 96% availability under severe conditions while meeting all integrity requirements.
机译:对于支持飞机精确进近和着陆的新的全天候导航辅助设备有强烈的需求。联邦航空局的局域增强系统(LAAS)就是这样一种导航辅助工具,它使用全球定位系统(GPS)来估计飞机的位置。要求LAAS提供非常高的准确性,完整性,连续性和可用性,并且在十亿次进近中一个未检测到的导航故障的完整性要求已成为该系统设计中的关键挑战。付出了巨大的努力,开发了各种方法来保证各种潜在异常的完整性,这些异常可能威胁到LAAS辅助着陆。当前,几乎所有这些风险都可以通过现有方法来缓解。剩下的一个问题是电离层异常引起的风险。本文介绍了利用GPS现代化技术对电离层异常进行完整性检测的新颖算法-GPS系统正在发生变化,以增强民用用户的能力。这种现代化包括添加新的GPS民用信号,这些信号使多频技术成为可能。这项研究集中于两种类型的双频载波平滑方法-无散度平滑和无电离层平滑-并开发了使用这些方法的电离层异常完整性算法。仿真显示,使用无电离层平滑的第一种算法最多可以在美国本土(CONUS)的广大区域实现96%至99.9%的可用性。对于实际使用而言,这种可用性水平低得令人无法接受。但是,好处是所得的可用性不是电离层条件的函数。仿真显示,第二种算法基于无散度平滑,在标称电离层条件下,超过70%的CONUS可获得99.9%以上的可用性。但是,它有可能在严重的电离层条件下完全失去可用性。利用这两种算法,本研究介绍了一种实现两种平滑方法的系统架构。最终的系统根据电离层监测器获得的当前电离层状态的最佳估计值来切换平滑方法,该监测器也作为本研究的一部分而设计。在满足所有完整性要求的情况下,该体系结构在标称电离层条件下可实现99.9%以上的可用性,在恶劣条件下可实现96%以上的可用性。

著录项

  • 作者

    Konno, Hiroyuki.;

  • 作者单位

    Stanford University.;

  • 授予单位 Stanford University.;
  • 学科 Engineering Aerospace.
  • 学位 Ph.D.
  • 年度 2008
  • 页码 218 p.
  • 总页数 218
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类 航空、航天技术的研究与探索;
  • 关键词

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