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Method and device for controlling aircraft for preset aircraft type based on communication and command vehicle

A technology for aircraft and command vehicles, applied in the field of electronics, can solve problems such as low control efficiency, and achieve the effects of improving control efficiency, avoiding uncertainty, and saving computation.

Inactive Publication Date: 2018-08-10
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 based on a communication command vehicle for a preset model, 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 for preset aircraft type based on communication and command vehicle
  • Method and device for controlling aircraft for preset aircraft type based on communication and command vehicle
  • Method and device for controlling aircraft for preset aircraft type based on communication and command vehicle

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Embodiment 1

[0069] The first aspect of the present invention provides a method for controlling an aircraft based on a communication command vehicle for a preset model, please refer to figure 1 , is a flowchart of a method for controlling an aircraft based on a communication command vehicle for a preset model in an embodiment of the present invention.

[0070] It should first be explained that the method can be applied to a communication command vehicle for controlling and monitoring an aircraft, or a ground station with a computer-operated control function (the ground station is a portable box with an integrated notebook computer built-in ), or a remote control terminal (such as control room, monitoring room, etc.). In other words, the above-mentioned steps in the embodiment of the present invention include the steps to be described below, and its executive body can be a communication command vehicle, so that the control method of the aircraft can be controlled in the vehicle, or it can b...

Embodiment approach

[0091] As an optional implementation manner, converting the current state information into a second physical control quantity includes:

[0092] Analyzing the correspondence between the current state information and the first physical control quantity;

[0093] According to the corresponding relationship, the current state information is converted into the second physical control quantity.

[0094] 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

[0096] Based on the same inventive concept as the method of controlling the aircraft based on the communication command vehicle for the preset model in the aforementioned first aspect, Embodiment 2 of the present invention also provides a control device for the aircraft, including:

[0097] The current geographic location coordinate acquisition module is used for the communication command vehicle to obtain the current geographic location coordinates of each of the aircraft in the plurality of aircraft;

[0098] The target area selection module is used for the communication command vehicle to select the target area to be controlled according to the current geographic location coordinates of each of the aircraft;

[0099] The target aircraft selection module is used for the communication command vehicle to select the target aircraft to be controlled according to the aircraft type in the target area, and the aircraft type is one of the following: fixed-wing aircraft, multi-rotor a...

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PUM

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Abstract

An embodiment of the invention provides a method for controlling an aircraft for a preset aircraft type based on a communication and command vehicle. The method comprises the following steps: the communication and command vehicle obtains a current geographic coordinate of each aircraft in a plurality of aircrafts; the communication and command vehicle selects a target area needing to be controlled, and selects a target aircraft needing to the controlled according to aircraft type; the communication and command vehicle obtains a first control instruction, and analyzes the first control instruction; the communication and command vehicle obtains current state information of the aircraft, and converts the current state information into a second physical control quantity; and the communicationand command vehicle obtains increment between a first physical control quantity and the second physical control quantity, and controls the aircraft based on the increment. Efficiency of the 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 based on a communication command vehicle for a preset model. 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 based...

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