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Method and device for controlling aircraft

A technology of aircraft and physical control, applied in the electronic field, can solve the problems of low control efficiency, achieve the effect of improving control efficiency, avoiding uncertainty, and saving calculation amount

Inactive Publication Date: 2018-07-24
EWATT TECH CO LTD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0005] The embodiment of the present invention provides a method and device for controlling an aircraft, which is used to solve the problem of low control efficiency in the method for controlling an aircraft in the prior art

Method used

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  • Method and device for controlling aircraft
  • Method and device for controlling aircraft
  • Method and device for controlling aircraft

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Experimental program
Comparison scheme
Effect test

Embodiment 1

[0065] The first aspect of the present invention provides a method for controlling an aircraft, please refer to figure 1 , is a flowchart of a method for controlling an aircraft in an embodiment of the present invention. The method includes:

[0066] S110: Obtain the current geographic location coordinates of each of the aircraft in the plurality of aircraft;

[0067] Specifically, this application is specifically used to control the aircraft that are flying in the air, and there will be multiple aircraft flying in the air at the same time, so when it is necessary to control a certain aircraft at this time, you can obtain the information of several aircraft through the preferred method. The current geographic location coordinates of each of the aircraft, and the aircraft that need to be controlled are screened according to the current geographic location coordinates of each of the aircraft;

[0068] S120: Select a target aircraft to be controlled according to the current geo...

Embodiment approach

[0084] As an optional implementation manner, converting the current state information into a second physical control quantity includes:

[0085] Analyzing the correspondence between the current state information and the first physical control quantity;

[0086] According to the corresponding relationship, the current state information is converted into the second physical control quantity.

[0087] For example, there will be a corresponding relationship between the current state information and the first physical control quantity, such as the relationship between velocity and angular acceleration, the relationship between deflection angle and angular velocity, and then the corresponding relationship is converted into an angular value by designing the controller. Acceleration value, that is, the second physical control quantity.

Embodiment 2

[0089] Based on the same inventive concept as the method for controlling the aircraft in the aforementioned first aspect, Embodiment 2 of the present invention also provides a control device for the aircraft, such as figure 2 shown, including:

[0090] The current geographic location coordinates acquisition module 210 is configured to acquire the current geographic location coordinates of each of the several aircrafts;

[0091] The target aircraft selection module 220 is used to select the target aircraft to be controlled according to the current geographic location coordinates of each of the aircraft;

[0092] The first obtaining module 230 is configured to obtain a first control instruction, the first control instruction is an original control instruction used to control the target aircraft to fly to a target state;

[0093] An analysis module 240, configured to analyze the first control instruction to obtain a first physical control quantity related to the control of the ...

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PUM

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Abstract

An embodiment of the present invention provides a method and device for controlling an aircraft. The method comprises a step of obtaining current geographic location coordinates of each aircraft in aplurality of aircrafts, a step of selecting a target aircraft which needs to be controlled according to the current geographic location coordinates of each aircraft, a step of obtaining a first control command which is an original control command used for controlling the aircraft to fly to a target state, a step of analyzing the first control command and obtaining a first physical control amount related to aircraft control, a step of obtaining current state information of the aircraft, a step of converting the current state information into a second physical control amount, and a step of obtaining an increment between the first physical control amount and the second physical control amount and controlling the aircraft based on the increment. According to the method and the device, the efficiency of an aircraft control method is improved.

Description

technical field [0001] The invention relates to the field of electronic technology, in particular to a method and device for controlling an aircraft. Background technique [0002] At present, aircraft are widely used in map surveying, forest surveying, disaster monitoring, logistics express, high-altitude photography and other fields. [0003] In the prior art, the method for controlling the aircraft generally controls the aircraft through the original control instructions set in the pre-model. However, since the control command changes at any time, the same method needs to be used to control the aircraft every time the control command changes, resulting in low control efficiency. [0004] It can be seen that there is a technical problem of low control efficiency in the prior art. Contents of the invention [0005] Embodiments of the present invention provide a method and device for controlling an aircraft, which are used to solve the problem of low control efficiency in...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G05D1/08G05D1/10
CPCG05D1/0808G05D1/101
Inventor 赵国成余辉叶宇鹰李少坤詹福宇
Owner EWATT TECH CO LTD