60.60 Standard published Aug 21, 2023
ISO
ISO/TC 20/SC 16 Unmanned aircraft systems
International Standard
49.020 Aircraft and space vehicles in general
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.
PUBLISHED
ISO 5110:2023
60.60
Standard published
Aug 21, 2023