An autonomous multi-rotor airplane comprises a body frame with a chamber. The chamber is configured to provide space for one or more skydivers or jumpers, a lifting platform having an onboard computer and an avionic system. The airplane comprises one or more propulsion systems operably coupled to the lifting platform. The airplane is configured to find and execute the optimal flight path based on given information by the operator. The airplane comprises one or more user interfaces securely positioned inside the chamber. The user interfaces are configured to enable the skydiver to view the location and the optimal flight path, and adjust the angle of the autonomous multi-rotor airplane against the wind direction. The user interface is configured to enable the skydiver to operate and land the autonomous multi-rotor airplane at a landing zone.
AUTONOMOUS MULTI-ROTOR AIRPLANE
2021-01-07
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
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