SRGPS稳健机载导航算法

M. Heo, B. Pervan, J. Gautier, S. Pullen, P. Enge, D. Gebre‐Egziabher
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引用次数: 22

摘要

舰载相对GPS (SRGPS)是联合精确进近和着陆系统(JPALS)的一种结构变体,为舰载自动着陆提供高精度和高完整性的DGPS导航。本文主要研究SRGPS终端导航的鲁棒机载算法设计。在这种情况下,定义了一种处理方法,以最佳地结合无几何滤波和几何冗余的互补优势。具体而言,当飞机远离船舶(SRGPS服务体积内或外)时,使用无几何滤波对宽频整数进行周期估计。对于双频实现,在SRGPS业务量进入之前进行码/载波无发散滤波的优势可能特别显著,因为可以使用较长的滤波持续时间。本文详细介绍了鲁棒导航体系结构,并结合飞机舰载降落的导航完整性要求对鲁棒导航体系结构的性能进行了评价。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Robust airborne navigation algorithms for SRGPS
Shipboard-relative GPS (SRGPS) is an architectural variant of the joint precision approach and landing system (JPALS) that provides high accuracy and high integrity DGPS navigation for automatic shipboard landings. This research is focused on the design of robust airborne algorithms for SRGPS terminal navigation. In this context, a processing methodology is defined to optimally combine the complementary benefits of geometry-free filtering and geometric redundancy. Specifically, when the aircraft is far from the ship (inside or outside the SRGPS service volume), geometry-free filtering is used for cycle estimation of widelane integers. For dual frequency implementations, the advantage of code/carrier divergence-free filtering prior to SRGPS service volume entry can be especially significant because long filter durations can be used. In this paper, the robust navigation architecture is detailed and its performance is evaluated relative to the navigation integrity requirements for shipboard landing of aircraft.
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