Unmanned aerial vehicle and method for safely landing an unmanned aerial vehicle
AssigneeAirbus Defence and Space GmbH
InventorManfred Hiebl
Life of this patent
Estimating the term…
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AssigneeAirbus Defence and Space GmbH
InventorManfred Hiebl
Estimating the term…
An unmanned aerial vehicle with lift and propulsion system and a flight control system and method. The flight control system has a flight control unit, a navigation system, a communication system and an actuator system. The flight control unit can calculate, based on data from the navigation system and/or data of a ground control station, control commands which can be fed to the actuator system for actuating the lift and propulsion system. The ground control station is configured to control and/or monitor the aerial vehicle. The aerial vehicle has a monitoring unit to monitor the communication system to determine whether all the communication links are interrupted. The monitoring unit can cause the flight control unit to land the aerial vehicle safely at a suitable landing site based on stored data relating to current flight conditions and nearby landing sites.
An unmanned aerial vehicle, comprising:
A method for safely landing an unmanned aerial vehicle, comprising:
A ground control station for controlling and/or monitoring at least one unmanned aerial vehicle, comprising:
Dependencies are inferred from the claim text.