ISO 5110:2023 风雨条件下多旋翼无人驾驶飞机系统飞行稳定性的试验方法

标准编号：ISO 5110:2023

中文名称：风雨条件下多旋翼无人驾驶飞机系统飞行稳定性的试验方法

英文名称：Test method for flight stability of a multi-copter unmanned aircraft system (UAS) under wind and rain conditions

发布日期：2023-08

标准范围

本文件规定了测试多旋翼无人驾驶飞机系统（UAS）飞行稳定性的程序，适用于可垂直起降的多旋翼型UAS。重量超过250的商用多直升机UAS？g到150以下？本文件讨论了kg。此外，本文件适用于军用和民用多直升机UAS。然而，本文件中未规定该检测的定量特异性稳定性标准。

This document specifies the procedures for testing flight stability of a multi-copter unmanned aircraft system (UAS) and is applicable to multi-copter type UAS that can take-off and land vertically. A commercial multi-copter UAS weighing over 250 g to less than 150 kg is discussed in this document. Further, this document is applicable to military and civilian multi-copter UAS. However, quantitatively specific stability criteria for the test are not specified in this document.

标准预览图