标准摘要
[中文适用范围]： 本文件规定了多旋翼无人机系统 (UAS) 飞行稳定性测试程序，适用于可垂直起飞和降落的多旋翼型 UAS。本文件讨论了重量超过 250 克至不到 150 公斤的商用多旋翼 UAS。此外，本文件适用于军用和民用多旋翼 UAS。但是，本文件未指定测试的定量具体稳定性标准。 [外文原描述]： 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.
英文名称Test method for flight stability of a multi-copter unmanned aircraft system (UAS) under wind and rain conditions