Résumé
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.
Informations générales
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État actuel: PubliéeDate de publication: 2023-10Stade: Norme internationale publiée [60.60]
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Edition: 1
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Comité technique :ISO/TC 20/SC 16ICS :49.020
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