Invention Grant
- Patent Title: Unmanned aircraft, device for controlling unmanned aircraft, method for controlling unmanned aircraft, and device for detecting failure of unmanned aircraft
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Application No.: US16469079Application Date: 2017-12-13
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Publication No.: US11640178B2Publication Date: 2023-05-02
- Inventor: Kenzo Nonami , Yi Yang
- Applicant: ACSL Ltd.
- Applicant Address: JP Tokyo
- Assignee: ACSL Ltd.
- Current Assignee: ACSL Ltd.
- Current Assignee Address: JP Tokyo
- Agency: McDonnell Boehnen Hullbert & Berghoff LLP
- Priority: JPJP2016-241718 20161213,JPJP2017-082315 20170418
- International Application: PCT/JP2017/044712 WO 20171213
- International Announcement: WO2018/110598 WO 20180621
- Main IPC: G05D1/08
- IPC: G05D1/08 ; B64C39/02 ; G05D1/00 ; G06F17/16 ; B64U10/10 ; B64U30/20 ; B64U101/00
Abstract:
[Problem to be Solved]
The object is to provide a device, a method and the like which, when a fault occurs, particularly when a fault occurs in an operation of some of rotary wings, can control a flight depending on the fault, or which can be at least used for control when a fault occurs, or which can detect the fault.
[Solution]
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.
The object is to provide a device, a method and the like which, when a fault occurs, particularly when a fault occurs in an operation of some of rotary wings, can control a flight depending on the fault, or which can be at least used for control when a fault occurs, or which can detect the fault.
[Solution]
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.
Information query
