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This document specifies the purpose, conditions and methods for the test of civil small multi-copter unmanned aircraft (UA) docking system, including the inspection of basic characteristics, functional test, performance test, environmental adaptability compatibility test, and electromagnetic compatibility test.
This document is applicable to docking systems of civil small multi-copter UA with maximum take-off mass (MTOM) level II through IV as defined in ISO 21895. The general requirements of civil small multi-copter UA docking system are documented in ISO 25215. Testing for other types of multi--copter UA docking systems might be performed in accordance with this document.
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