60.60 Standard published May 12, 2023
ISO
ISO/TC 20/SC 16 Unmanned aircraft systems
International Standard
49.020 Aircraft and space vehicles in general
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.
PUBLISHED
ISO 24355:2023
60.60
Standard published
May 12, 2023