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Evaluation method for the resonance frequency of the multi-copter UA (unmanned aircraft) by measurement of rotor and body frequencies
60.60 Standard published
Test method for flight stability of a multi-copter unmanned aircraft system (UAS) under wind and rain conditions
60.60 Standard published
Flight performance of civil small and light fixed-wing unmanned aircraft systems (UAS) — Test methods
60.60 Standard published
Civil small and light unmanned aircraft systems (UAS) — Vibration test methods
60.60 Standard published
Civil small and light unmanned aircraft (UA) — Sharp injury to human body by rotor blades — Evaluation and test method
60.60 Standard published
Civil small and light unmanned aircraft systems (UAS) under low-pressure conditions — Test methods
60.60 Standard published
Detection and avoidance systems for uncrewed aircraft systems
50.20 Proof sent to secretariat or FDIS ballot initiated: 8 weeks
Unmanned aircraft systems — Part 3: Operational procedures
30.60 Close of voting/ comment period
Unmanned aircraft systems — Part 4: Vocabulary
50.00 Final text received or FDIS registered for formal approval
Categorization and classification of civil unmanned aircraft systems
30.99 CD approved for registration as DIS
Survey for operational procedure for Airspace Conflict Management
30.99 CD approved for registration as DIS
Survey on functional and performance requirements of UTM systems
30.99 CD approved for registration as DIS
Unmanned aircraft systems — Training for personnel involved in UAS operations
30.60 Close of voting/ comment period
Civil small and light unmanned aircraft systems (UAS) under high-temperature and low-temperature conditions — Test methods
00.60 Close of review
Test methods for civil small and light multi-copter unmanned aircraft dock system
30.60 Close of voting/ comment period
Unmanned aircraft systems — General requirements and test methods for the hydrogen fuel gas pipes of gaseous hydrogen fuel cell powered UAV
30.60 Close of voting/ comment period
Unmanned aircraft systems — General requirements and test methods for the attachable hydrogen cylinders of gaseous hydrogen fuel cell powered UAV
30.60 Close of voting/ comment period
