A control device for unmanned aircraft comprising: a rotary-wing control signal generation circuit for generating a rotary wing control signal for causing a driving device to drive a plurality of rotary wings for flying the unmanned aircraft; a measuring device for measuring a physical amount relating to an operation of at least one of the plurality of rotary wings; and a fault detection circuit for detecting a fault in the operation of at least one of the plurality of rotary wings by using the physical amount measured by the measuring device, wherein the rotary-wing control signal generation circuit is configured to generate a rotary wing control signal depending on the fault detected by the fault detection circuit in the operation of at least one of the plurality of rotary wings, is provided.
Unmanned Aircraft, Device for Controlling Unmanned Aircraft, Method for Controlling Unmanned Aircraft, and Device for Detecting Failure of Unmanned Aircraft
2020-04-02
Patent
Electronic Resource
English
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