Flight performance of civil small and light fixed-wing unmanned aircraft systems (UAS). Test methods

Flight performance of civil small and light fixed-wing unmanned aircraft systems (UAS). Test methods

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1   Scope

This document specifies the test requirements and methods for verifying the specified flight performance items of civil fixed-wing unmanned aircraft systems (UAS).
This document is applicable to the category of civil small and light fixed-wing UAS, which applies to maximum take-off mass (MTOM) level I through V according to ISO 21895.