Performance de vol des aéronefs sans pilote (UAS) civils petits et légers à voilure fixe — Méthodes d'essais

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.