超视距飞行研究的AirSTAR硬件和软件设计

S. Laughter, D. Cox
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引用次数: 1

摘要

美国国家航空航天局(NASA)机载次尺度运输机研究(AirSTAR)无人机系统(UAS)是一种用于研究紧急情况下车辆飞行动力学的设施,以支持航空安全研究。该系统经过升级,其操作范围大大扩大,超出了地面飞行员的视线范围。对机载飞行硬件进行了重新设计,并对软件基础进行了重大更改,以提供适当的自主行为,以应对一些潜在的故障和危险。地面硬件和系统监视器也进行了升级,包括冗余通信链路,包括基于ADS-B的位置显示和独立的飞行终端系统。该设计包括定制和商用航空电子设备,结合在一起,允许飞行实验设计的灵活性,同时仍然受益于在返航模式下的测试配置。在软件架构中采用了类似的层次结构,以允许对研究代码进行测试,并退回到更彻底验证的飞行控制。作为远程驾驶设施,地面系统也被开发,以确保飞行模式和系统状态实时传达给地面操作人员。本文概述了超视距飞行作战的概念,并对机载硬件和软件设计进行了详细的回顾。本次讨论是在安全和程序要求的背景下进行的,这些要求推动了AirSTAR无人机超视距能力的许多设计决策。
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AirSTAR hardware and software design for beyond visual range flight research
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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