DocumentCode :
3394344
Title :
The NASA Langley Research Center´s Unmanned Aerial System Surrogate research aircraft
Author :
Howell, Charles T., III ; Jessup, Artie ; Jones, Frank ; Joyce, Claude ; Sugden, Paul ; Verstynen, Harry ; Mielnik, John
Author_Institution :
Langley Res. Center, NASA, Hampton, VA, USA
fYear :
2010
fDate :
3-7 Oct. 2010
Abstract :
Research is needed to determine what procedures, aircraft sensors and other systems will be required to allow Unmanned Aerial Systems (UAS) to safely operate with manned aircraft in the National Airspace System (NAS). The NASA Langley Research Center has transformed a Cirrus Design SR22 general aviation (GA) aircraft into a UAS Surrogate research aircraft to serve as a platform for UAS systems research, development, flight testing and evaluation. The aircraft is manned with a Safety Pilot and systems operator that allows for flight operations almost anywhere in the NAS without the need for a Federal Aviation Administration (FAA) Certificate of Authorization (COA). The UAS Surrogate can be controlled from a modular, transportable ground station like a true UAS. The UAS Surrogate is able to file and fly in the NAS with normal traffic and is an ideal platform for real world UAS research and development compared to actual UAS flying in restricted ranges or other sterilized airspace. The Cirrus Design SR22 aircraft is a small, single-engine, four-place, composite-construction aircraft that NASA Langley acquired to support NASA flight-research programs like the Small Aircraft Transportation System (SATS) Project. Systems were installed to support flight test research and data gathering. These systems include: separate research power; multi-function flat-panel displays; research computers; research air data and inertial state sensors; video recording; data acquisition; datalink; S-band video and data telemetry; Common Airborne Instrumentation System (CAIS); Automatic Dependent Surveillance-Broadcast (ADS-B); instrumented surfaces and controls; and a systems operator work station. The transformation of the SR22 to a UAS Surrogate was accomplished in phases. The first phase was to modify the existing autopilot to accept external commands from a research computer that was connected by redundant data-link radios to a ground control station. An electro-mechanical auto-throttle - - was added in the next phase to provide ground station control of airspeed. Additional phases are in progress to add waypoint navigation and long range satellite voice and data communications. Potential areas for UAS Surrogate research include the development, flight test and evaluation of sensors to aid in the process of air traffic “detect-sense-and-avoid”. These sensors could be evaluated in real-time and compared with onboard human evaluation pilots. This paper describes the systems and design considerations that were incorporated in the development of the UAS Surrogate along with details of development problems encountered and the corresponding solutions.
Keywords :
air safety; air traffic control; aircraft control; aircraft displays; aircraft testing; data acquisition; remotely operated vehicles; sensors; surveillance; telemetry; video recording; CAIS; COA; Cirrus Design SR22 general aviation aircraft; Federal Aviation Administration; GA aircraft; NASA Langley Research Center; National Airspace System; S-band video telemetry; UAS Surrogate research aircraft; air traffic; aircraft sensor; automatic dependent surveillance-broadcast; certificate of authorization; common airborne instrumentation system; data acquisition; flight testing; ground station control; inertial state sensor; multifunction flat-panel display; research computer; safety pilot; safety system; unmanned aerial system; video recording; Aerospace electronics; Aircraft; Aircraft manufacture; Aircraft navigation; Computers; NASA; Servomotors;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Digital Avionics Systems Conference (DASC), 2010 IEEE/AIAA 29th
Conference_Location :
Salt Lake City, UT
ISSN :
2155-7195
Print_ISBN :
978-1-4244-6616-0
Type :
conf
DOI :
10.1109/DASC.2010.5655303
Filename :
5655303
Link To Document :
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