发明名称 PRECISION APPROACH GUIDANCE SYSTEM AND ASSOCIATED METHOD
摘要 A precision approach guidance system that provides flying craft guidance information during a precision approach to a landing site and methods associated therewith are provided. In one embodiment, the system includes: an inertial navigation system, an onboard ranging sensor, a terrain database storing previously identified position-referenced terrain information associated with the landing site, and a position determining process. The position determining process repetitively determines a corrected position of the flying craft during the precision approach based at least in part on attitude and velocity information from an inertial navigation system, current position-referenced terrain information based on measurements from an onboard ranging sensor, and previously identified position-referenced terrain information from the terrain database.
申请公布号 WO2007067192(A3) 申请公布日期 2007.12.27
申请号 WO2006US02329 申请日期 2006.01.24
申请人 OHIO UNIVERSITY;CAMPBELL, JACOB L.;VAN GRAAS, FRANK;DE HAAG, MAARTEN UIJT 发明人 CAMPBELL, JACOB L.;VAN GRAAS, FRANK;DE HAAG, MAARTEN UIJT
分类号 G01S13/91;G06F19/00 主分类号 G01S13/91
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