ISO 5110:2023 PDF
Test method for flight stability of a multi-copter unmanned aircraft system (UAS) under wind and rain conditions
Open preview (PDF)Test method for flight stability of a multi-copter unmanned aircraft system (UAS) under wind and rain conditionsTitle (English):
ISO 5110:2023
Test method for flight stability of a multi-copter unmanned aircraft system (UAS) under wind and rain conditions
- Document status:
- Active
- Format:
- Electronic (PDF)
- Number of pages:
- 20
- Publication date:
- August 21, 2023
- Edition:
- ISO IS 5110 edition 1 version 1
- ICS:
- 49.020
Description (English):
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.
Technical details
- Technical committee
- ISO/TC 20/SC 16 - Unmanned aircraft systems
- SKU
- ISO 5110:2023
