ISO 5309:2023 民間小型軽量無人航空機システム (UAS) | ページ 2

Foreword

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This document was prepared by Technical ISO/TC 20, Aircraft and space vehicles, Subcommittee SC 16, Unmanned aircraft systems.

Introduction

In recent years, the market for lightweight and small civil unmanned aircraft systems (UAS) has developed rapidly. Application areas range from consumer-grade unmanned aircraft vehicles fitted with a camera to industrial-grade unmanned aircraft vehicles used in various safety and inspection operations (e.g. in agriculture, electrical distribution and public safety). As a consequence of being transported from job site to job site, the UAS is exposed to a vibration environment during its lifetime. This document sets out a vibration environment that reflects the situation the UAS experiences during transportation and flight, and to which it can be tested so as to verify whether the test article complies with the applicable performance standards (excluding durability requirements) when subjected to vibration levels specified for the appropriate installation.

1 Scope

This document specifies the test conditions and methods to be used for the vibration testing of unmanned aircraft system (UAS, including unmanned aircraft and ground station) which applies to level II through V according to ISO 21895.

2 Normative references

The following documents are referred to in the text in such a way that some or all of their content constitutes requirements of this document. For dated references, only the edition cited applies. For undated references, the latest edition of the referenced document (including any amendments) applies.

3 Terms and definitions

For the purposes of this document, the terms and definitions given in ISO 2041 and ISO 21384-4 and the following apply.

ISO and IEC maintain terminology databases for use in standardization at the following addresses:

Bibliography