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System Design of a FMCW Radar-Based Detect-and-Track Subsystem for an Airborne Detect-and-Avoid System On-Board of Small Unmanned Aircraft Systems

机译:基于FMCW雷达的检测和轨道子系统的系统设计,用于空降检测和避免小型无人机系统车载系统

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This paper describes and evaluates an all-weather capable detect-and-track subsystem based on a miniaturized frequency-modulated continuous-wave radar sensor operating between 23.55 and 24.4 GHz. This radar sensor was designed to detect obstacles like other airspace participants on board of a small unmanned aircraft system (sUAS) during automated flights. The radar consists of one transmit and four receiver patch-antennae arrays, which are placed in a square formation close to the transmitting antenna array. By evaluating the time-of-arrival parameter from a pair of two vertically displaced antenna arrays the calculation of the elevation angle becomes possible. In addition, the azimuth angle is calculated the same way using the alternative horizontally displaced patch-antenna array couple. Thus, the received radar signals can be used for detection and tracking of targets in three-dimensional space. A specific constant false alarm rate (CFAR) has been implemented, which applies an appropriate threshold that maximizes the probability of detections and keeps the probability of false alarm below a preset level. First flight tests were carried out to validate this radar prototype and its target detection and tracking capabilities as a subsystem of a radar-based detect-and-avoid system (DAA), suitable to be installed on board of small unmanned aircraft systems.
机译:本文介绍基于在23.55和24.4GHz之间的小型化频调制的连续波雷达传感器的基于小型化频调制的连续波雷达传感器的全天候能力的检测和轨道子系统。该雷达传感器旨在在自动航班期间检测小型无人机系统(SUAS)的其他空域参与者的障碍物。雷达包括一个发射和四个接收器贴片天线阵列,其被放置在靠近发送天线阵列的方形形成中。通过从一对两个垂直移位的天线阵列中评估到达时间参数,所以升降角的计算变得可能。另外,使用替代水平移位的贴片天线阵列耦合来计算方位角的方式相同。因此,所接收的雷达信号可用于检测和跟踪三维空间中的目标。具体恒虚警率(CFAR)已经执行,它适用最大化检测的概率,并保持低于预设电平假警报的概率的适当阈值。进行第一次飞行测试以验证该雷达原型及其目标检测和跟踪能力作为基于雷达的检测和避免系统(DAA)的子系统,适用于小型无人机系统的船上。

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