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Vision-assisted miniature unmanned aerial vehicle indoor flight three-dimensional attitude algorithm

A technology of three-dimensional attitude and UAV, which is applied in the field of UAV, and can solve the problems of magnetometer application limitation, UAV attitude calculation interference, and accuracy reduction.

Pending Publication Date: 2020-04-17
北京智新翼行科技有限公司
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Problems solved by technology

However, due to the limitations of its own size, weight and computing power, micro-UAVs cannot use navigation sensors with higher requirements for volume, weight and power consumption, and visual navigation algorithms with a large amount of calculation to achieve indoor autonomous flight.
At the same time, the indoor magnetic field environment is complex, and the application of the magnetometer in the room is greatly limited. The attitude calculation of the UAV will be disturbed, the accuracy will be reduced, and even the heading angle calculation will be wrong.

Method used

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  • Vision-assisted miniature unmanned aerial vehicle indoor flight three-dimensional attitude algorithm
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Embodiment Construction

[0083] The present invention will be described in detail in conjunction with accompanying drawing now. This figure is a simplified schematic diagram only illustrating the basic structure of the present invention in a schematic manner, so it only shows the components relevant to the present invention.

[0084] Such as figure 1 As shown, a kind of vision-assisted micro-UAV indoor flight three-dimensional attitude algorithm of the present invention includes the solution of the three-dimensional attitude angle of the drone under the normal magnetic field environment, and performs calculations on the horizontal attitude angle and heading angle during the calculation process. Decoupling; the calculation of the three-dimensional attitude angle of the UAV in an abnormal magnetic field environment; and the correction of the heading angle of the corridor flight visual aid; in this embodiment, the vision module uses a forward-looking monocular camera, and the pictures collected by the ca...

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Abstract

The invention provides a vision-assisted miniature unmanned aerial vehicle indoor flight three-dimensional attitude algorithm. Pure autonomous calculation of a pitch angle, a roll angle and a course angle during indoor flight of an unmanned aerial vehicle can be realized. When the data of a magnetometer is valid, the three-dimensional attitude of the unmanned aerial vehicle is resolved by utilizing the data of an IMU and the magnetometer, and the resolving of a horizontal attitude angle and the resolving of a course angle are decoupled; when data of the magnetometer fails, only IMU data is used for achieving three-dimensional attitude calculation, the influence of the accelerometer on course angle calculation is cut off, and it is ensured that the precision requirement of course angle calculation within the endurance time is met without assistance of the magnetometer; and when the unmanned aerial vehicle flies in an indoor corridor, a forward-looking monocular camera module is used forachieving narrow channel detection, the angle of the unmanned aerial vehicle deviating from the corridor line is extracted, and the accumulated error of the course angle of the unmanned aerial vehicle is corrected through extended Kalman filtering according to the deviation angle.

Description

technical field [0001] The invention relates to the technical field of unmanned aerial vehicles, in particular to a three-dimensional attitude algorithm for indoor flight of a visually assisted micro unmanned aerial vehicle. Background technique [0002] Due to its small size, light weight and concealment, micro drones are very suitable for flying applications in indoor environments, such as indoor reconnaissance, search and rescue, and environmental detection. However, due to the limitations of its own size, weight and computing power, micro-UAVs cannot use navigation sensors with higher requirements for size, weight and power consumption, and visual navigation algorithms with a large amount of calculation to achieve indoor autonomous flight. At the same time, the indoor magnetic field environment is complex, and the application of the magnetometer in the room is greatly limited. The attitude calculation of the UAV will be disturbed, the accuracy will be reduced, and even t...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G01C21/20
CPCG01C21/206
Inventor 李德辉王冠林史海庆邓成端
Owner 北京智新翼行科技有限公司