ISO 5286:2023

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

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.

OEN:

ISO

Langue:

English

Code(s) de l'ICS:

49.020

Statut:

Publié

Date de Publication:

2023-10-22

Numéro Standard:

ISO 5286:2023