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Detect-and-Avoid Safety and Operational Suitability Analysis using an Electro-Optical/Infared Sensor ModelThis report documents a closed-loop analysis of an DAA system using a Electro/Optical sensor model. Safety and operational suitability metrics are computed. Results show that the safety metrics are most sensitive to the angular rate accuracy of the intruder aircraft. Trade-off between safety and operationl suitability metrics is discussed. Results from this work directly inform the requirements of an electro/optical sensors for detect-and-avoid.
Document ID
20210016872
Acquisition Source
Ames Research Center
Document Type
Technical Memorandum (TM)
Authors
Christine Serres
(MIT Lincoln Laboratory Lexington, Massachusetts, United States)
Bilal Gill
(MIT Lincoln Laboratory Lexington, Massachusetts, United States)
Matthew W M Edwards
(MIT Lincoln Laboratory Lexington, Massachusetts, United States)
Gilbert Wu
(Ames Research Center Mountain View, California, United States)
Date Acquired
June 3, 2021
Publication Date
June 30, 2021
Publication Information
Publisher: NASA
Subject Category
Air Transportation And Safety
Report/Patent Number
NASA/TM-20210016872
Funding Number(s)
CONTRACT_GRANT: NASA
Distribution Limits
Public
Copyright
Portions of document may include copyright protected material.
Technical Review
NASA Technical Management
Keywords
Detect-and-avoid
DAA
Electro-Optical/Infared
EO/IR
Unmanned Aviation Systems in the National Airspace
UAS-NAS
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