DSF/ISO/DIS 24355
General requirements of flight control system for civil small and light multirotor UAS
inactive
| Organization: | DS |
| Status: | inactive |
| Page Count: | 14 |
| ICS Code (Aircraft and space vehicles in general): | 49.020 |
scope:
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 flight. The flight control system in this document consists of flight control unit, navigation unit, fault diagnosis and management unit, flight planning, flight recorder, etc. The design and manufacture for other UA flight control systems or subsystems may refer to this document.
Document History
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...
DSF/ISO/DIS 24355
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...