ISO-5110 › Test method for flight stability of a multi-copter unmanned aircraft system (UAS) under wind and rain conditions

ISO-5110 - 1ST EDITION - CURRENT


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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.

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Document Number

ISO 5110:2023

Revision Level

1ST EDITION

Status

Current

Publication Date

Aug. 1, 2023

Committee Number

ISO/TC 20/SC 16