ISO 5110:2023
Test method for flight stability of a multi-copter unmanned aircraft system (UAS) under wind and rain conditions
OVERVIEW
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.
COMMENTS
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PRODUCT DETAILS
| Status | Current |
|---|---|
| Edition | 2023 |
| No. of Pages | 20 |
| ICS Classification | 49.020 Aircraft and space vehicles in general |
| Committee | ISO/TC 20/SC 16 |
| Available for Purchase | For sale in Singapore only |
| Adoption | ISO |