Publication Date:
2019-07-20
Description:
In support of NASAs 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.
Keywords:
Aircraft Design, Testing and Performance
Type:
NF1676L-28544
,
2018 AIAA Aviation Forum; Jun 25, 2018 - Jun 29, 2018; Atlanta, GA; United States
Format:
application/pdf
