ISO 5110:2023 PDF
Test method for flight stability of a multi-copter unmanned aircraft system (UAS) under wind and rain conditions
Название (английский):
ISO 5110:2023
Test method for flight stability of a multi-copter unmanned aircraft system (UAS) under wind and rain conditions
- Статус документа:
- Действующий
- Формат:
- Электронный (PDF)
- Количество страниц:
- 20
- Дата публикации:
- 21 августа 2023 г.
- Издание:
- ISO IS 5110 edition 1 version 1
- ICS:
- 49.020
Описание (английский):
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.
Технические детали
- Технический комитет
- ISO/TC 20/SC 16 - Unmanned aircraft systems
- SKU
- ISO 5110:2023