ISO 5110:2023
p
ISO 5110:2023
80802

Status : Published

en
Format Language
std 1 129 PDF + ePub
std 2 129 Paper
  • CHF129
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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.

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General information

  •  : Published
     : 2023-08
    : International Standard published [60.60]
  •  : 1
     : 20
  • ISO/TC 20/SC 16
    49.020 
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