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Airborne stabilization mechanism for unmanned aerial vehicle

A drone and stability technology, applied in aircraft stability, aircraft parts, aircraft control, etc., can solve the problems of high production cost, large volume and weight, complex structure, etc., and achieve low production cost, high measurement and control accuracy, and low profile Effect

Inactive Publication Date: 2019-05-21
XIAN AISHENG TECH GRP +1
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Query existing patents, papers and other public technical documents related to UAV airborne stabilization equipment, most of which are three-axis or polar coordinate turntables with complex structures, high production costs, large volume and weight, and are not suitable for low-cost small UAVs

Method used

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  • Airborne stabilization mechanism for unmanned aerial vehicle
  • Airborne stabilization mechanism for unmanned aerial vehicle
  • Airborne stabilization mechanism for unmanned aerial vehicle

Examples

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Embodiment Construction

[0021] The embodiments described below by referring to the figures are exemplary and are intended to explain the present invention and should not be construed as limiting the present invention.

[0022] In describing the present invention, it should be understood that the terms "center", "longitudinal", "transverse", "length", "width", "thickness", "upper", "lower", "front", " Orientation indicated by rear, left, right, vertical, horizontal, top, bottom, inside, outside, clockwise, counterclockwise, etc. The positional relationship is based on the orientation or positional relationship shown in the drawings, which is only for the convenience of describing the present invention and simplifying the description, rather than indicating or implying that the referred device or element must have a specific orientation, be constructed and operated in a specific orientation, Therefore, it should not be construed as limiting the invention.

[0023] see figure 1 , in this embodiment, t...

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Abstract

The invention provides an airborne stabilization mechanism for an unmanned aerial vehicle. The airborne stabilization mechanism includes an upper platform, a lower platform, an actuator, a mechanism controller and joints; a mechanism controller fixed on the lower platform senses the attitude change of the unmanned aerial vehicle, based on this, the length of a push rod is changed by controlling the actuator which is fixedly connected through the lower platform through the three single-degree-of-freedom joints, an upper platform connected with the actuator through three double-degree-freedom joints is driven, the attitude change, in a space, of the upper platform just counteracts the attitude change of the unmanned aerial vehicle, a load fixedly connected with the upper platform can still keep spatial balance and stability when the unmanned aerial vehicle bumps and sways, thus the vibration intensity of the load of the upper platform is effectively reduced, and the spatial stability ofthe load is improved. The digital control mechatronic integrated stabilization mechanism based on the modern measurement and control principle has the obvious advantages of advanced technology and high precision and is suitable for various types of unmanned aerial vehicles and small aircrafts.

Description

technical field [0001] The invention belongs to the technical field of industrial automation control, and in particular relates to a high-performance, low-cost UAV airborne stabilization mechanism, which is suitable for the popularization and application of various types of UAVs and small aircraft, and avoids or reduces the turbulence of the UAV itself The effect of sloshing on loads attached to the platform. Background technique [0002] There are various mission loads of UAVs, and their effects are related to their own accuracy and the peripheral environment. Generally, mission loads have corresponding requirements for the flight characteristics of UAVs, especially requiring UAVs to maintain a certain attitude stability during flight. However, this puts forward strict requirements on the UAV body, which cannot be fully realized in many cases. [0003] The loads of existing small and medium-sized UAVs are mostly fixedly connected to the UAV. When the UAV is violently bumpe...

Claims

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Application Information

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IPC IPC(8): B64C17/00
Inventor 张剑锋乔冰介苏朋侯泊江吴玉生
Owner XIAN AISHENG TECH GRP
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