An integrated electric steering gear for unmanned aerial vehicles

An electric steering gear and integrated technology, which is applied in the direction of aircraft transmission, aircraft power transmission, aircraft power device, etc., can solve the problems of unsatisfactory rapidity and high reliability, poor environmental adaptability, poor control accuracy, etc., and achieve Satisfy the effect of continuous long-term work, improve life and reliability, and improve sealing

Active Publication Date: 2017-04-05
BEIJING RES INST OF PRECISE MECHATRONICS CONTROLS
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

The traditional electric steering gear for drones uses DC brushed motors as the power source, and multi-stage pinions as the transmission deceleration mechanism, which has small load moment, short life cycle, poor environmental adaptability, and poor control accuracy (between 0.15° and 0.2° Between) and other shortcomings, can not meet the requirements of rapidity and high reliability

Method used

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  • An integrated electric steering gear for unmanned aerial vehicles
  • An integrated electric steering gear for unmanned aerial vehicles
  • An integrated electric steering gear for unmanned aerial vehicles

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Embodiment Construction

[0046] The basic idea of ​​the present invention is: the electric steering gear of the present invention includes two parts, the steering gear and the control driver, and the steering gear and the control driver are designed in an integrated manner. The steering gear is composed of a DC brushless motor, planetary reducer, hollow angular displacement sensor, output rocker, etc.; the control drive is composed of a control board and a driving board. The structure diagram is as follows: figure 2 shown.

[0047] It is specifically applied in the field of UAV rudder surface control. The DC brushless motor is used as the power source, and the scheme of connecting the DC brushless motor, planetary reducer, and hollow angular displacement sensor in series makes the structure of the steering gear compact and reduces its space. size, and improve its working life and reliability; the steering gear housing adopts a sealed structure design, which has strong dustproof and waterproof capabil...

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Abstract

The invention discloses an integrated electric actuator for an unmanned aerial vehicle, which is specifically applied to the field of control surface control for unmanned aerial vehicles. According to the scheme, a brushless direct-current motor is used as a power source, and due to the scheme of serially connecting the brushless direct-current motor, a planetary reducer and a hollow angular displacement sensor, the actuator is compact in structure, and the spatial dimensions thereof are reduced, the working life thereof is prolonged, and the reliability thereof is improved; a shell of the actuator adopts a sealed structure design, and is high in dustproof and waterproof capacities, and adaptive to bad working environments; a control driver adopts the control strategy of a position and two-stage current limiting, a current-limiting ring is mainly used for limiting an excessive current occurring in a system under abnormal conditions, and protecting the safety of the electric actuator and the unmanned aerial vehicle; and with regard to a square-wave position angle instruction, real-time acquisition for the angle instruction is realized by means of interrupt capture, and the accuracy of acquisition for the angle instruction is improved by adopting the control strategy of angle amplitude-limiting filtering and instruction compensation, therefore, the accuracy of the flight attitude of the unmanned aerial vehicle can be greatly improved, and can achieve 0.1 degrees.

Description

technical field [0001] The invention relates to an integrated electric steering gear for an unmanned aerial vehicle, belonging to the technical field of unmanned aerial vehicle control surface control. Background technique [0002] With the rapid development of unmanned aerial vehicles, in order to meet the increasing reliability and light weight of unmanned aerial vehicles and other technical requirements, higher requirements are put forward for the electric steering gear, which is an important part of unmanned aerial vehicles. As the actuator of the UAV control system, the electric steering gear is one of the key executive components of the UAV. It is mainly used to control the angle of the rudder surface of the UAV to adjust the UAV's deflection, pitch, roll and other attitudes. Its working performance and reliability directly affect the control accuracy and working reliability of the UAV's flight attitude. [0003] A lot of research has been done on the UAV steering sys...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64C13/50
Inventor 李怀兵晋华峰徐豪榜聂振金陆豪
Owner BEIJING RES INST OF PRECISE MECHATRONICS CONTROLS
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