Analysis of Influence of UAS Speed Range and Turn Performance on Detect and Avoid Sensor Requirements

Jack, Devin P ; Hardy, Jeremy S ; Hoffler, Keith D

关键词: LOW WEIGHT;    NATIONAL AIRSPACE SYSTEM;    PILOTLESS AIRCRAFT;    SYSTEMS INTEGRATION;    UNMANNED AIRCRAFT SYSTEMS;    SYSTEMS;   

RP-ID  :  NF1676L-28544

学科分类：航空航天科学

美国|英语

来源: NASA Technical Reports Server

【 摘 要 】

In support of NASA’s Unmanned Aircraft Systems Integration in the National Airspace System project and RTCA Special Committee 228, an analysis has been performed to provide insight in to the trade space between unmanned aircraft speed and turn capability and detect and avoid sensor range requirements. The work was done as an initial part of the effort to understand low size, weight, and power sensor requirements for aircraft that have a limited speed envelope or can limit the envelope for portions of their mission and may be able to turn at higher than “standard rate.” Range and timeline reductions coming from limiting speed range and from increasing available turn rate in some speed ranges are shown.