AirSTAR hardware and software design for beyond visual range flight research

2016 IEEE/AIAA 35th Digital Avionics Systems Conference (DASC)(2016)

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摘要
The National Aeronautics and Space Administration (NASA) Airborne Subscale Transport Aircraft Research (AirSTAR) Unmanned Aerial System (UAS) is a facility developed to study the flight dynamics of vehicles in emergency conditions, in support of aviation safety research. The system was upgraded to have its operational range significantly expanded, going beyond the line of sight of a ground-based pilot. A redesign of the airborne flight hardware was undertaken, as well as significant changes to the software base, in order to provide appropriate autonomous behavior in response to a number of potential failures and hazards. Ground hardware and system monitors were also upgraded to include redundant communication links, including ADS-B based position displays and an independent flight termination system. The design included both custom and commercially available avionics, combined to allow flexibility in flight experiment design while still benefiting from tested configurations in reversionary flight modes. A similar hierarchy was employed in the software architecture, to allow research codes to be tested, with a fallback to more thoroughly validated flight controls. As a remotely piloted facility, ground systems were also developed to ensure the flight modes and system state were communicated to ground operations personnel in real-time. Presented in this paper is a general overview of the concept of operations for beyond visual range flight, and a detailed review of the airborne hardware and software design. This discussion is held in the context of the safety and procedural requirements that drove many of the design decisions for the AirSTAR UAS Beyond Visual Range capability.
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关键词
AirSTAR hardware,software design,visual range flight research,National Aeronautics and Space Administration,NASA,airborne subscale transport aircraft research,unmanned aerial system,UAS,flight dynamics,emergency conditions,aviation safety research,ground-based pilot,airborne flight hardware,autonomous behavior,redundant communication links,ADS-B based position displays,independent flight termination system,commercially available avionics,validated flight controls,remotely piloted facility,flight modes,ground operations personnel,procedural requirements,visual range capability
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