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ISO 24355:2023

Current Revision

Flight control system for civil small and light multicopter unmanned aircraft system (UAS) - General requirements

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This document specifies the composition, functional and performance requirements of flight controls for civil multicopter unmanned aircrafts (UAs) with the maximum take-off mass (MTOM) less than or equal to 25 kg corresponding to unmanned aircraft systems (UAS) at levels I, II, III and IV as graded in ISO 21895 which does not include fully autonomous flights.

The flight control system in this document consists of flight control unit, navigation unit, fault diagnosis and management unit, flight planning, flight recorder, etc. This document is applicable to the design and manufacture of other UA flight control systems or subsystems.


SDO ISO: International Organization for Standardization
Document Number ISO 24355
Publication Date Not Available
Language en - English
Page Count
Revision Level
Supercedes
Committee ISO/TC 20/SC 16
Publish Date Document Id Type View
Not Available ISO 24355:2023 Revision