小型无人机航电传感器融合感知与规避

S. Ramasamy, R. Sabatini, A. Gardi
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引用次数: 61

摘要

合作和非合作感知和避免(SAA)系统是无人机(UA)常规进入非隔离空域的关键使能器。本文研究了小型UA应用中一些最新的协作式和非协作式传感器和系统技术,并讨论了相关的多传感器数据融合技术。非合作传感器包括被动和主动前视传感器(FLS)和合作系统包括交通碰撞避免系统(TCAS),自动相关监视广播(ADS-B)系统和/或模式C转发器是提议的SAA架构的一部分。在介绍了SAA系统流程的基础上,提出了数据融合的关键数学模型。使用交互多模型(IMM)算法来估计入侵者的状态向量,并利用概率模型将其传播到预测未来的轨迹。采用这些数学模型,确定了合作入侵者和非合作入侵者的冲突检测和解决策略。此外,还进行了详细的误差分析,以确定入侵者轨道周围空域的总体不确定性。这是通过考虑影响测量的导航和跟踪误差并将其转换为统一的距离和方位不确定性描述符来实现的,该描述符适用于合作和非合作场景。详细的仿真案例研究进行了评估所提出的SAA方法在代表性主机平台(AEROSONDE UA)和各种入侵平台(包括大型运输机和其他UA)上的性能。结果表明,当SAA工艺在超过500米的范围内进行时,始终保持所需的安全分离距离。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Avionics sensor fusion for small size unmanned aircraft Sense-and-Avoid
Cooperative and non-cooperative Sense-and-Avoid (SAA) systems are key enablers for Unmanned Aircraft (UA) to routinely access non-segregated airspace. In this paper some state-of-the-art cooperative and non-cooperative sensor and system technologies are investigated for small size UA applications, and the associated multisensor data fusion techniques are discussed. Non-cooperative sensors including both passive and active Forward Looking Sensors (FLS) and cooperative systems including Traffic Collision Avoidance System (TCAS), Automatic Dependent Surveillance - Broadcast (ADS-B) system and/or Mode C transponders are part of the proposed SAA architecture. After introducing the SAA system processes, the key mathematical models for data fusion are presented. The Interacting Multiple Model (IMM) algorithm is used to estimate the state vector of the intruders and this is propagated to predict the future trajectories using a probabilistic model. Adopting these mathematical models, conflict detection and resolution strategies for both cooperative and un-cooperative intruders are identified. Additionally, a detailed error analysis is performed to determine the overall uncertainty volume in the airspace surrounding the intruder tracks. This is accomplished by considering both the navigation and the tracking errors affecting the measurements and translating them to unified range and bearing uncertainty descriptors, which apply both to cooperative and non-cooperative scenarios. Detailed simulation case studies are carried out to evaluate the performance of the proposed SAA approach on a representative host platform (AEROSONDE UA) and various intruder platforms, including large transport aircraft and other UA. Results show that the required safe separation distance is always maintained when the SAA process is performed from ranges in excess of 500 metres.
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