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Unmanned Aerial Vehicle Flight Control System and Steering Gear Positioning Module

A flight control system, unmanned aerial vehicle technology, applied in aircraft control, aircraft parts, aircraft transmission and other directions, can solve installation obstacles, unmanned aerial vehicle transportation, inconvenient launch and other problems

Active Publication Date: 2021-07-30
成都云鼎智控科技有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

At present, for UAVs that are long in shape and usually fly along their own length direction, the propulsion system and rudder system are usually set far apart in the length direction of UAVs, which is easy for UAVs. The installation of other functional components creates obstacles, and it also brings inconvenience to the transportation and launch of UAVs

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  • Unmanned Aerial Vehicle Flight Control System and Steering Gear Positioning Module

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Embodiment Construction

[0020] The present invention will be clearly and completely described below in conjunction with the accompanying drawings. Those skilled in the art will be able to implement the present invention based on these descriptions. Before the present invention is described in conjunction with the accompanying drawings, it should be pointed out that:

[0021] The technical solutions and technical features provided in each part of the present invention, including the following description, can be combined with each other under the condition of no conflict.

[0022] In addition, the embodiments of the present invention involved in the following descriptions are usually only a part of the embodiments of the present invention rather than all the embodiments. Therefore, based on the embodiments of the present invention, those skilled in the art will not make any All other embodiments obtained under the premise of creative labor shall belong to the protection scope of the present invention. ...

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Abstract

The invention discloses a flight control system of an unmanned aerial vehicle and a steering gear positioning module. The flight control system of the unmanned aerial vehicle includes: a main control system, a propulsion system, a rudder system, and a feedback system; the propulsion system has at least two ducts in total. The fan propulsion unit, the rudder system has at least three steering gears in total, the at least two ducted fan propulsion units and the at least three steering gears are collectively arranged at the tail of the unmanned aerial vehicle, and the rudder system also includes steering gears The positioning module, the steering gear positioning module includes the steering gear installation and positioning reference shaft located in the housing at the tail of the unmanned aerial vehicle and the spoke-shaped assembly connected to the steering gear installation and positioning reference shaft through the first radial positioning structure and the first circumferential positioning structure. The positioning component, the spoke-shaped positioning component is installed on the tail end of the main structure of the unmanned aerial vehicle through the second radial positioning structure and the second circumferential positioning structure, and at least three steering gears are respectively positioned and installed on the steering gear installation and positioning reference axis corresponding to Servo installation part.

Description

technical field [0001] The invention relates to a flight control system of an unmanned aerial vehicle, which mainly includes a main control system, a propulsion system, a rudder system and a feedback system. Background technique [0002] The flight control system of UAV usually includes main control system, propulsion system, rudder system and feedback system. Among them, the propulsion system is used to provide thrust to keep the UAV flying; the rudder system is used to realize the steering of the UAV; the main control system is used to control the operation of the propulsion system and the rudder system; the feedback system is used to feed back to the main control system Control results for unmanned aerial vehicles. The UAV flight control system needs to match the type of UAV. At present, for UAVs that are long in shape and usually fly along their own length direction, the propulsion system and rudder system are usually set far apart in the length direction of UAVs, whic...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64C19/00B64C13/50
CPCB64C13/50B64C19/00
Inventor 唐冰刘以建
Owner 成都云鼎智控科技有限公司
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