BS ISO 5286:2023

Flight performance of civil small and light fixed-wing unmanned aircraft systems (UAS). Test methods. | Status: Current

1 Scope This document specifies the test requirements and methods for verifying the specified flight performance items of civil fixed-wing unmanned aircraft systems (UAS). This document is applicable to the category of civil small and light fixed-wing UAS, which applies to maximum take-off mass (MTOM) level I through V according to ISO 21895.