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Aerial vehicle and control method thereof and computer readable storage medium

An aircraft and processor technology, applied in the field of aircraft, can solve problems such as aircraft crashes, aircraft unable to receive driving signals in real time and continuously, and unable to output driving signals, so as to achieve the effect of ensuring continuity

Inactive Publication Date: 2018-11-30
BEIJING SANKUAI ONLINE TECH CO LTD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, through a processor to output the drive signal, when the processor fails, the drive signal cannot be output, resulting in the crash of the aircraft
[0003] At present, although some aircrafts are equipped with two processors, there will still be situations where the aircraft cannot receive the driving signals in real time and continuously, which will cause the aircraft to crash

Method used

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  • Aerial vehicle and control method thereof and computer readable storage medium
  • Aerial vehicle and control method thereof and computer readable storage medium
  • Aerial vehicle and control method thereof and computer readable storage medium

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Embodiment Construction

[0044] Reference will now be made in detail to the exemplary embodiments, examples of which are illustrated in the accompanying drawings. When the following description refers to the accompanying drawings, the same numerals in different drawings refer to the same or similar elements unless otherwise indicated. The implementations described in the following exemplary examples do not represent all implementations consistent with the present disclosure. Rather, they are merely examples of apparatuses and methods consistent with aspects of the present disclosure as recited in the appended claims.

[0045] figure 1 It is a schematic structure diagram of an aircraft according to an embodiment of the present invention. The aircraft shown in this embodiment can be an unmanned aerial vehicle, such as figure 1 As shown, the aircraft includes:

[0046] At least two processors: processor 1A and processor 1B. It should be noted that, figure 1 The illustrated embodiment illustrates the...

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Abstract

The invention relates to an aerial vehicle. The aerial vehicle comprises at least two processors and gate module, wherein each processor of the at least two processors simultaneously outputs a drivingsignal after the aerial vehicle is started; the gate module is used for receiving driving signals of the at least two processors and selecting a driving signal generated by a non-abnormal processor from the received driving signals and transmitting the driving signal to a motor of the. aerial vehicle. According to the aerial vehicle, no time interval exists when the motor of the unmanned aerial vehicle receives the driving signal, so that the problem that the motor of the aerial vehicle cannot receive the driving signal in the process that the gating module stops transmitting the driving signal output by a first processor to the motor of the aerial vehicle and transmits the driving signal output by a non-abnormal second processor of the at least two processors to the motor of the aerial vehicle can be solved, continuity of the work of the motor can be ensured, and the problem caused by the motor stopping of the aerial vehicle can be solved.

Description

technical field [0001] The present disclosure relates to the technical field of aircraft, and in particular to an aircraft, an aircraft control method, and a computer-readable storage medium. Background technique [0002] Conventional aircraft such as drones output driving signals through a processor to drive components such as rotors to work. However, if a processor outputs the drive signal, when the processor fails, the drive signal cannot be output, resulting in a crash of the aircraft. [0003] At present, although some aircrafts are equipped with two processors, there are still situations where the aircraft cannot receive the driving signals in real time and continuously, resulting in the crash of the aircraft. Contents of the invention [0004] The present disclosure provides an aircraft, an aircraft control method, and a computer-readable storage medium. [0005] According to a first aspect of the present disclosure, an aircraft is proposed, comprising: [0006] ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G05B9/03
CPCG05B9/03
Inventor 贾泽浩刘宝旭
Owner BEIJING SANKUAI ONLINE TECH CO LTD