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A flight controller and its auxiliary flight control method

A flight controller and controller technology, applied in the field of flight controllers, can solve the problems of remote control aircraft survey and exploration, and achieve the effect of improving work efficiency

Active Publication Date: 2018-06-01
SUZHOU INST OF INDAL TECH
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] Aircraft operators often need to go through a lot of time and debugging to master and be proficient in the control of various aircraft, which makes it difficult to apply remote control aircraft to survey and exploration.

Method used

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  • A flight controller and its auxiliary flight control method
  • A flight controller and its auxiliary flight control method
  • A flight controller and its auxiliary flight control method

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Embodiment Construction

[0035] In order to make the object, technical solution, and advantages of the present invention clearer, the specific implementation manners of the present invention will be described in detail below in conjunction with the accompanying drawings.

[0036] The technical solutions in the embodiments of the present invention will be clearly and completely described and discussed below in conjunction with the accompanying drawings of the present invention. Obviously, what is described here is only a part of the examples of the present invention, not all examples. Based on the present invention All other embodiments obtained by persons of ordinary skill in the art without creative efforts fall within the protection scope of the present invention.

[0037] The four-blade aircraft has four groups of DC motors as the power to rise, wherein two groups of rotors (propellers) rotate clockwise, and the other two groups rotate counterclockwise. The purpose is to use the reaction forces pro...

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PUM

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Abstract

The invention discloses a flight controller, which includes a single-chip microcomputer, a propeller motor, an auxiliary flight controller, a power supply module, a wireless receiving module, an image sensor, a wireless sending module and a PWM signal four-channel output module; the auxiliary flight controller includes a PI controller , gyroscope, accelerometer, analog-to-digital converter; power supply module, PI controller, single-chip microcomputer, PWM signal four-channel output module are connected sequentially; gyroscope, accelerometer are connected with analog-to-digital converter, analog-to-digital converter The PI controller is connected, and the wireless receiving module, image sensor, and wireless sending module are all connected to the single-chip microcomputer; the power supply module is connected to the image sensor; the four-channel output module is connected to the control circuit of the propeller motor of the flight controller. The invention enables the aircraft to be used in surveying, detection, monitoring and other occasions, and an auxiliary flight controller is installed on the aircraft so that the aircraft can maintain a stable attitude and a fixed heading.

Description

technical field [0001] The invention relates to the field of remote control flight control, in particular to a flight controller with an auxiliary flight controller. Background technique [0002] In the prior art, the remote-controlled aircraft must be fully concentrated during operation. Taking the four-blade aircraft as an example, the main reason is that the rotation of the wings during the flight of the aircraft provides the buoyancy of the aircraft, and the rotation of the rotor simultaneously provides the buoyancy of the aircraft. At the same time, the action force and reaction force generated by the rotation of the rotor will affect the attitude and heading of the aircraft, and when the operating place is located outdoors, the aircraft will be affected by wind and airflow. Therefore, the operator of the flight remote controller has to focus on the attitude, heading, position, altitude and other states of the aircraft at any time, and make corrections and stabilize the...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G05D1/10
Inventor 刘训非祝清兰凌璟
Owner SUZHOU INST OF INDAL TECH
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