DS/ISO 24355
Flight control system for civil small and light multicopter unmanned aircraft system (UAS) – General requirements
active, Most Current
| Organization: | DS |
| Publication Date: | 16 May 2023 |
| Status: | active |
| Page Count: | 18 |
| ICS Code (Aircraft and space vehicles in general): | 49.020 |
scope:
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.
Document History
DS/ISO 24355
May 16, 2023
Flight control system for civil small and light multicopter unmanned aircraft system (UAS) – General requirements
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...
General requirements of flight control system for civil small and light multirotor UAS
This standard specifies the composition, functional, and performance requirements of flight controls for civil multicopper UAS with MTOM from 250g to 25kg which does not include fully autonomous...