This part of GB/T38924 specifies the vibration test requirements and methods for civil light and small unmanned aerial vehicles (takeoff weight 0.25kg ~ 150kg) system (including aircraft and ground stations), including test conditions, test equipment and instruments, test process, Test interruption and recovery, test result evaluation and test report, etc. This section applies to civilian light and small (maximum take-off weight greater than 0.25kg and not greater than 150kg) multi-rotor UAV systems, fixed-wing UAV systems, unmanned helicopter systems and Vehicle-mounted ground station to determine whether civilian light and small unmanned aerial vehicle systems can withstand the impact of vibration environments.
GB/T 38924.6-2020 Referenced Document
GB/T 35018 Classification and grading for civil unmanned aircraft system
GB/T 38924.6-2020 history
2020GB/T 38924.6-2020 Environmental test methods for civil small and light unmanned aircraft system—Part 6: Vibration test