ISO 5110:2023

Published (Edition 1, 2023)

ISO 5110:2023

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Abstract

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.

General information

Status
: Published

Publication date
: 2023-08

Stage
: International Standard published [60.60]
Edition
: 1

Number of pages
: 20
Technical Committee :
ISO/TC 20/SC 16

ICS :
49.020
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