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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 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:
This document is applicable to the design and manufacture of other UA flight control systems or subsystems.
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