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A semi-autonomous ground imitation flight system and control method for unmanned aerial vehicles

A control method and flight controller technology, applied in control/regulation systems, non-electric variable control, three-dimensional position/course control, etc., can solve problems such as unstable altitude control, barometer data interference, and susceptibility to interference, and achieve The effect of convenient operation

Active Publication Date: 2019-11-22
BEIJING BOYING TONGHANG TECH CO LTD
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] 1. The barometer calculates the altitude of the current location by obtaining the air pressure value of the current location, but due to the change of the air pressure around the drone caused by the maneuvering of the drone, the obtained altitude may not be accurate
[0004] 2. When flying near the ground, the influence of the wind field formed by the UAV and the ground has a great interference on the barometer data
[0005] 3. Unable to perceive the change of surface altitude, follow the terrain to fly
To a certain extent, it can solve the problem of UAV flying near the surface of the ground, but the update rate of the ultrasonic sensor is slow, susceptible to interference, and the noise is large. The altitude control under the ground (such as cornfields, wheat fields, bushes, etc.) is unstable and cannot be applied to industrial drones with large loads

Method used

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  • A semi-autonomous ground imitation flight system and control method for unmanned aerial vehicles
  • A semi-autonomous ground imitation flight system and control method for unmanned aerial vehicles
  • A semi-autonomous ground imitation flight system and control method for unmanned aerial vehicles

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Embodiment Construction

[0024] The present invention will be further described below in conjunction with the accompanying drawings and embodiments.

[0025] A semi-autonomous ground imitation flight system for unmanned aerial vehicles, such as figure 1 As shown, it includes GPS positioning module, inertial measurement module, barometer module, radar altimeter, motor driver, propeller power structure and flight controller,

[0026] The GPS positioning module is connected to the flight controller through the UART interface, the inertial measurement module is connected to the flight controller through the SPI interface, the radar altimeter is connected to the flight controller through the UART interface, and the motor driver is connected to the flight controller through the PWM interface. The output shaft is connected to the power structure of the propeller, and the flight controller obtains the data of the GPS positioning module, the inertial measurement module and the radar altimeter to calculate the ...

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Abstract

The invention relates to a semi-autonomous imitation terrain flight system of an unmanned aerial vehicle. The semi-autonomous imitation terrain flight system comprises a GPS (global positioning system) positioning module, an inertia measurement module, a barometer module, a radar height meter, a motor driver, a paddle power structure and a flight controller, and is characterized in that the flight controller obtains data of the GPS positioning module, the inertia measurement module and the radar height meter to perform fusion algorithm calculation; position, posture and height data of the unmanned aerial vehicle is obtained, so that the motor driver is controlled, and accordingly the unmanned aerial vehicle can perform imitation terrain flight along a flight course in a semi-autonomous mode.

Description

technical field [0001] The invention relates to an automatic flight control system for an unmanned aerial vehicle, in particular to a semi-autonomous ground imitation flight system and a control method for an unmanned aerial vehicle. Background technique [0002] The altitude control of UAV is a difficult point in the field of UAV, especially the imitation flight near the surface. General drone altitude control calculates the current altitude of the drone through the fusion of barometer and accelerometer. The problems with this approach are: [0003] 1. The barometer calculates the altitude of the current location by obtaining the air pressure value of the current location, but due to the change of the air pressure around the drone caused by the maneuvering of the drone, the obtained altitude may not be accurate [0004] 2. When flying near the ground, the influence of the wind field formed by the UAV and the ground has a great interference on the barometer data [0005] ...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G05D1/10
CPCG05D1/101
Inventor 曾龙王飞张继孝崔利刘志军林劲
Owner BEIJING BOYING TONGHANG TECH CO LTD