全球导航卫星系统应用
导线
航空航天工程
计算机科学
路径(计算)
航空学
工程类
大地测量学
地质学
卫星
程序设计语言
作者
Robert J. Kelly,Jerald M. Davis
标识
DOI:10.1002/j.2161-4296.1994.tb02320.x
摘要
A methodology to determine the required navigation performance (RNP) for aircraft precision approach and landing under instrument meteorological conditions (IMC) is described. The RNP in turn defines an aircraft containment surface about the nominal flight path, called a tunnel, which specifies the allowed approach and landing flight path limits. If the aircraft and its navigation system satisfy the RNP, then the aircraft will successfully traverse the tunnel, terminating in a safe landing. The tunnel is defined by four RNP parameters: accuracy, integrity, continuity, and availability.
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