ISO 5109:2023
p
ISO 5109:2023
80801
Status : Published
en
Format Language
std 1 61 PDF + ePub
std 2 61 Paper
  • CHF61
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Abstract

This document provides a method for evaluating the resonance vibration frequency of the multi-copter unmanned aircraft (UA). This document specifies a method of designing the UA so as to avoid the resonance generated by the coincidence of the natural frequency of the UA body and the rotational frequency of the rotor.

This document is applicable to multi-copter UA weighing less than 150 kg.

General information

  •  : Published
     : 2023-07
    : International Standard published [60.60]
  •  : 1
     : 9
  • ISO/TC 20/SC 16
    49.020 
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