DocumentCode :
2536452
Title :
Simulation and flight test capability for testing prototype sense and avoid system elements
Author :
Howell, C.T. ; Stock, T.M. ; Wehner, P.J. ; Verstynen, H.A.
Author_Institution :
NASA Langley Res. Center, Hampton, VA, USA
fYear :
2012
fDate :
14-18 Oct. 2012
Abstract :
NASA Langley Research Center (LaRC) and The MITRE Corporation (MITRE) have developed - and successfully demonstrated - an integrated simulation-to-flight capability for evaluating sense and avoid (SAA) system elements. This integrated capability consists of a MITRE developed fast-time computer simulation for evaluating SAA algorithms, and a NASA LaRC surrogate unmanned aircraft system (UAS) equipped to support hardware and software in-the-loop evaluation of SAA system elements (e.g., algorithms, sensors, architecture, communications, autonomous systems), concepts, and procedures. The fast-time computer simulation subjects algorithms to simulated flight encounters/ conditions and generates a fitness report that records strengths, weaknesses, and overall performance. Reviewed algorithms (and their fitness report) are then transferred to NASA LaRC where additional (joint) airworthiness evaluations are performed on the candidate SAA system-element configurations, concepts, and/or procedures of interest; software and hardware components are integrated into the Surrogate UAS´ research systems; and flight safety and mission planning activities are completed. Onboard the Surrogate UAS, candidate SAA system element configurations, concepts, and/or procedures are subjected to flight evaluations and in-flight performance is monitored. The Surrogate UAS, which can be controlled remotely via generic Ground Station uplink or automatically via onboard systems, operates with a NASA Safety Pilot/Pilot in Command onboard to permit safe operations in mixed airspace with manned aircraft. An end-to-end demonstration of a typical application of the capability was performed in non-exclusionary airspace in October 2011; additional research, development, flight testing, and evaluation efforts using this integrated capability are planned throughout fiscal year 2012 and 2013.
Keywords :
aerospace safety; aerospace simulation; aircraft testing; autonomous aerial vehicles; MITRE corporation; NASA LaRC; NASA Langley Research Center; NASA safety pilot-pilot; SAA system-element configurations; UAS; airworthiness evaluations; fast-time computer simulation; fitness report; flight safety activity; flight test capability; generic ground station uplink; hardware components; hardware in-the-loop evaluation; in-flight performance; integrated simulation-to-flight capability; manned aircraft; mission planning activity; mixed airspace; nonexclusionary airspace; prototype sense testing; sense and avoid system elements; simulation test capability; software components; software in-the-loop evaluation; surrogate UAS; unmanned aircraft system; Aircraft; Algorithm design and analysis; Atmospheric modeling; Computational modeling; Heuristic algorithms; NASA; Software algorithms;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Digital Avionics Systems Conference (DASC), 2012 IEEE/AIAA 31st
Conference_Location :
Williamsburg, VA
ISSN :
2155-7195
Print_ISBN :
978-1-4673-1699-6
Type :
conf
DOI :
10.1109/DASC.2012.6382430
Filename :
6382430
Link To Document :
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