NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Design, Development, and Testing of a UAV Hardware-in-the-Loop Testbed for Aviation and Airspace Prognostics ResearchThe airspace is becoming more and more complicated, and will continue to do so in the future with the integration of Unmanned Aerial Vehicles (UAVs), autonomy, spacecraft, other forms of aviation technology into the airspace. The new technology and complexity increases the importance and difficulty of safety assurance. Additionally, testing new technologies on complex aviation systems & systems of systems can be very difficult, expensive, and sometimes unsafe in real life scenarios. Prognostic methodology provides an estimate of the health and risks of a component, vehicle, or airspace and knowledge of how that will change over time. That measure is especially useful in safety determination, mission planning, and maintenance scheduling. The developed testbed will be used to validate prediction algorithms for the real-time safety monitoring of the National Airspace System (NAS) and the prediction of unsafe events. The framework injects flight related anomalies related to ground systems, routing, airport congestion, etc. to test and verify algorithms for NAS safety. In our research work, we develop a live, distributed, hardware-in-the-loop testbed for aviation and airspace prognostics along with exploring further research possibilities to verify and validate future algorithms for NAS safety. The testbed integrates virtual aircraft using the X-Plane simulator and X-PlaneConnect toolbox, UAVs using onboard sensors and cellular communications, and hardware in the loop components. In addition, the testbed includes an additional research framework to support and simplify future research activities. It enables safe, accurate, and inexpensive experimentation and research into airspace and vehicle prognosis that would not have been possible otherwise. This paper describes the design, development, and testing of this system. Software reliability, safety and latency are some of the critical design considerations in development of the testbed. Integration of HITL elements in the development phases and veri cation/ validation are key elements to this report.
Document ID
20160013264
Acquisition Source
Ames Research Center
Document Type
Conference Paper
Authors
Kulkarni, Chetan
(SGT, Inc. Moffett Field, CA, United States)
Teubert, Chris
(SGT, Inc. Moffett Field, CA, United States)
Gorospe, George
(SGT, Inc. Moffett Field, CA, United States)
Burgett, Drew
(Christopher Newport Univ. Newport News, VA, United States)
Quach, Cuong C.
(NASA Langley Research Center Hampton, VA, United States)
Hogge, Edward
(Northrop Grumman Technical Services Hampton, VA, United States)
Date Acquired
November 4, 2016
Publication Date
June 13, 2016
Subject Category
Avionics And Aircraft Instrumentation
Report/Patent Number
ARC-E-DAA-TN32370
Funding Number(s)
CONTRACT_GRANT: NNA14AA60C
CONTRACT_GRANT: NNL12AA09C
CONTRACT_GRANT: NNX13AM40A
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
HITL
Vitual Aircraft
LVC-DE
No Preview Available