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Monocular Ranging for Small Unmanned Aerial Systems in the Far-Field Recent proliferation of small Unmanned Aerial Systems (sUAS) applications requires onboard collision avoidance systems to mitigate the risk of collision with non-cooperative aircraft and manned aircraft, which may not see sUAS in time to perform an avoidance maneuver. An attractive avenue for onboard collision avoidance is the utilization of machine vision cameras due to their low size, weight and power (SWaP) requirements. In this paper, we characterize the range performance of a machine vision system developed in-house and mounted onto an sUAS. The technique was designed to estimate the performance of a sense-and-avoid system to ensure that the sensing components meet the well-clear requirements for the chosen platform and avoidance strategy. Experimental flight-test data was acquired from test-flights flown along multiple collision geometries for two intruders: a general Aviation (GA) aircraft and a fixed-wing sUAS. The ownship and both intruders were instrumented with inertial navigation systems (INS) recording position and attitude information. The range at first detection, π‘ΉπŸŽ, was extracted from in-flight imagery of head-on collision course geometry synchronized with INS data from both aircraft and ground-truth values extracted from the raw imagery. This initial detection distance, π‘ΉπŸŽ, scales with atmospheric attenuation. Therefore, under clear sky conditions, the derived π‘ΉπŸŽ value represents the upper bound on the detection range achievable by the test configuration of the detector. Results indicate that the maximum initial detection distance for a 4k resolution action camera fitted with a 41ΒΊ Field of View (FOV) lens is 2.763 Β± 0.037 km for a GA aircraft and 0.881 Β± 0.061 km for a fixed-wing sUAS, respectively. The in results this study suggest that a vision-based detect and track system may be analyzed using the sensor characterization and contextualized within aircraft well-clear volumes.
Document ID
20205011011
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Chester V. Dolph
(Langley Research Center Hampton, Virginia, United States)
Cyrus Minwalla
(Scoped Systems)
Louis J. Glaab
(Langley Research Center Hampton, Virginia, United States)
B. Danette Allen
(Langley Research Center Hampton, Virginia, United States)
Khan M. Iftekharuddin
(Old Dominion University Norfolk, Virginia, United States)
Date Acquired
December 3, 2020
Subject Category
Avionics And Aircraft Instrumentation
Meeting Information
Meeting: AIAA SciTech Forum
Location: Online
Country: US
Start Date: January 11, 2021
End Date: January 23, 2021
Sponsors: AIAA
Funding Number(s)
WBS: 533127.02.60.07
Distribution Limits
Public
Copyright
Portions of document may include copyright protected material.
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