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.
Status: PublishedPublication date: 2023-08
Edition: 1Number of pages: 20
Technical Committee: ISO/TC 20/SC 16 Unmanned aircraft systems
Buy this standard
|std 1 124||PDF + ePub|
|std 2 124||Paper|