Design And Flight Test Of A Differential Gps Inertial Navigation System For Approach Landing Guidance

L Vallot,Scott D Snyder,Brian W Schipper,Nigel Parker,Cary R Spitzer

INSTITUTE OF NAVIGATION : PROCEEDINGS OF THE NATIONAL TECHNICAL MEETING : USING SYNERGISM TO STRENGTHEN NAVIGATION SYSTEMS（1991）

引用 21|浏览2

暂无评分

摘要

A flight test project evaluating an integrated differential GPS (DGPS)/inertial navigation system as an approach/landing aid has recently been completed. The test objectives were to acquire a system performance database, and to demonstrate automatic landings using the integrated DGPS/inertial system augmented with barometric and radar altimeters.

查看译文

关键词

inertial navigation,global positioning system,computer aided design,data bases

AI 理解论文

溯源树

样例

生成溯源树，研究论文发展脉络

Chat Paper

正在生成论文摘要