Résumé
PrévisualiserThis 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.
-
État actuel: PubliéeDate de publication: 2023-08
-
Edition: 1
-
- ICS :
- 49.020 Aéronautique et espace en général
Acheter cette norme
fr
| Format | Langue | |
|---|---|---|
| std 1 124 | PDF + ePub | |
| std 2 124 | Papier |
- CHF124
Cycle de vie
Vous avez une question?
Consulter notre FAQ
Service à la clientèle
+41 22 749 08 88
Horaires d’ouverture:
De lundi à vendredi - 09:00-12:00, 14:00-17:00 (UTC+1)