scope:

This document specifies the system test methods for civil multi-copter unmanned aircraft system. This document is intended to be a general standard for the test of the overall system UAS functionality with the support of subsystem. This document is applicable to the category of civil lightweight and small (maximum take-off weight under 150 kg) electric multi-copter unmanned aircraft system (UAS in short) . Configuration control and subsystem tests are important topics to be considered, but out of the scope of the file. The subsystem test like energy system and flight control system tests can be referred to other documents. The specified test methods can also be applied to the other categories as reference.