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Method and apparatus of controlling unmanned planes on account of model

A technology for drones and models, applied in the field of electronics, can solve problems such as poor stability and robustness, and achieve the effect of improving stability and robustness and solving poor stability.

Inactive Publication Date: 2018-07-10
EWATT TECH CO LTD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0005] Embodiments of the present invention provide a method and device for controlling UAVs based on models, which are used to solve the problems of poor stability and robustness in the methods for controlling UAVs based on models in the prior art. question

Method used

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  • Method and apparatus of controlling unmanned planes on account of model
  • Method and apparatus of controlling unmanned planes on account of model
  • Method and apparatus of controlling unmanned planes on account of model

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Embodiment 1

[0083] The first aspect of the present invention provides a method for controlling the UAV according to the model, please refer to figure 1 , is a flow chart of a method for controlling an unmanned aerial vehicle for a model in an embodiment of the present invention. The method includes:

[0084] S110: Obtain the current geographic location coordinates of each of the drones in several drones;

[0085] S120: Select a target area to be controlled according to the current geographic location coordinates of each of the drones;

[0086] S130: In the target area, select the target UAV that needs to be controlled according to the UAV type, and the UAV type is one of the following: fixed-wing UAV, multi-rotor UAV or unmanned helicopters;

[0087] Specifically, according to the current geographic location coordinates of each of the drones, selecting the target area to be controlled specifically includes the following sub-steps: according to the current geographic location coordinate...

Embodiment 2

[0127] Based on the same inventive concept as the method for controlling a drone in the aforementioned first aspect, Embodiment 2 of the present invention also provides a control device for a drone, such as figure 2 shown, including:

[0128] The current geographic location coordinates acquisition module is used to acquire the current geographic location coordinates of each of the drones in several drones;

[0129] A target area selection module, configured to select a target area to be controlled based on the current geographic location coordinates of each of the drones;

[0130] The target drone selection module is used to select the target drone that needs to be controlled according to the drone model in the target area, and the drone model is one of the following: fixed-wing unmanned aerial vehicles drones, multi-rotor UAVs or unmanned helicopters;

[0131] The first obtaining module is used to obtain the first control instruction, and the first control instruction is t...

Embodiment 3

[0149] Based on the same inventive concept as the method for controlling the drone in the first embodiment, the third embodiment of the present invention also provides a computer-readable storage medium, such as figure 2 As shown, there is stored thereon a computer program which, when executed by a processor, implements the following steps:

[0150] Acquiring the current geographic location coordinates of each of the drones in the plurality of drones;

[0151] Select a target area to be controlled according to the current geographic location coordinates of each of the drones;

[0152] In the target area, select the target UAV that needs to be controlled according to the UAV type, and the UAV type is one of the following: fixed-wing UAV, multi-rotor UAV or unmanned aerial vehicle man helicopter;

[0153] Obtaining a first control instruction, the first control instruction is an original control instruction used to control the target UAV to fly to a target state;

[0154] conv...

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Abstract

The embodiment of the invention provides a method and apparatus of controlling unmanned planes on account of model. The method of controlling an unmanned plane on account of model includes the steps:acquiring the current geographical position coordinates of each unmanned plane among a plurality of unmanned planes; according to the current geographical position coordinates of each unmanned plane,selecting the target area requiring controlling; according to the model of the unmanned plane, selecting a target unmanned plane requiring controlling in the target area; acquiring a first control command; according to a preset ideal model, converting the first control command into a second control command conforming the expected response dynamic state; acquiring the flight state parameters of theunmanned plane related with the second control command, and according to the flight state parameters, generating comprehensive feedback; according to the second control command and the comprehensivefeedback, performing error controlling so as to obtain a third control command; and according to the third control command, controlling the unmanned plane. The method and apparatus of controlling unmanned planes on account of model can realize the technical effect of improving stability and robustness of the unmanned plane control method.

Description

technical field [0001] The invention relates to the field of electronic technology, in particular to a method and a device for controlling an unmanned aerial vehicle for a model. Background technique [0002] At present, drones are widely used in map surveying, forest surveying, disaster monitoring, logistics express, high-altitude photography and other fields. [0003] The aircraft is essentially a complex nonlinear system. The traditional control method is to first linearize the mathematical model of the aircraft to obtain the linearized state equations of small disturbances in different modes, and then design corresponding control laws for different flight modes and carry out Adjust the parameters, and finally connect all the flight states to form the control law in the entire envelope. In the traditional control method, if the attitude of the aircraft changes drastically or is subject to large external interference, the aircraft cannot be effectively controlled, and it ...

Claims

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Application Information

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IPC IPC(8): G05D1/10
CPCG05D1/101
Inventor 赵国成余辉叶宇鹰李少坤詹福宇
Owner EWATT TECH CO LTD
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