A control system of a flight vehicle automatically varies the relationship between the center of gravity and the center of pressure of the flight vehicle. The control system automatically adjusts a center of pressure of the flight vehicle depending on a varying payload or payload type that is removably couplable to the flight vehicle. The control system automatically limits translational movement of the one or more wings of the flight vehicle in response to coupling of a payload to a fuselage of the flight vehicle.
Flight vehicle wing positioning system
2020-06-16
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
AUTONOMOUS FLIGHT VEHICLE CAPABLE OF FIXED WING FLIGHT AND ROTARY WING FLIGHT
European Patent Office | 2018
|Autonomous flight vehicle capable of fixed wing flight and rotary wing flight
European Patent Office | 2020
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