Résumé
This document specifies the procedures for testing flight stability of a multi-copter unmanned aircraft system (UAS) and is applicable to multi-copter type UAS that can take-off and land vertically. A commercial multi-copter UAS weighing over 250 g to less than 150 kg is discussed in this document. Further, this document is applicable to military and civilian multi-copter UAS. However, quantitatively specific stability criteria for the test are not specified in this document.
Informations générales
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État actuel: PubliéeDate de publication: 2023-08Stade: 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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