Control method and device for tilt rotorcraft

A technology of a tilt-rotor aircraft and a control method, which is applied in the field of aerodynamics and can solve the problems of increased model construction, confusion of control methods, difficulties, etc.

Active Publication Date: 2016-07-13
SHENYANG SHANGBO ZHITUO TECH CO LTD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Since the tiltrotor contains three flight modes, coupled with the confusion of control method

Method used

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  • Control method and device for tilt rotorcraft
  • Control method and device for tilt rotorcraft
  • Control method and device for tilt rotorcraft

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Embodiment Construction

[0040] The specific embodiments of the present invention will be described in detail below with reference to the accompanying drawings. It should be understood that the specific embodiments described here are only used to illustrate and explain the present invention, and are not used to limit the present invention.

[0041] figure 2 It is a flowchart of a method for controlling a tilt rotor aircraft provided by an exemplary embodiment. Such as figure 2 As shown, the control method of the tilt rotor aircraft may include the following steps.

[0042] In step S11, a dynamic reference model of the tiltrotor aircraft is established.

[0043] In step S12, a control system for controlling the tilt rotor aircraft is designed according to the reference model.

[0044] In step S13, the system state of the tiltrotor aircraft and the model difference between the reference model and the actual model are determined according to the reference model.

[0045] In step S14, the control system is oper...

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PUM

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Abstract

The invention discloses a control method and device for a tilt rotorcraft. The control method comprises steps of: establishing a dynamics reference model of the tilt rotorcraft; according to the reference model, designing a control system for controlling the tilt rotorcraft; according to the reference model, determining the system state of the tilt rotorcraft and a model difference between the reference model and an actual model; operating the control system according to the system state to obtain an virtual control input; correcting the virtual control input according to the model difference to obtain an actual control input; controlling the flight of the tilt rotorcraft according to the actual control input. Thus, the corrected actual control input is used for controlling the motion of the tilt rotorcraft so that the flight of the tilt rotorcraft is stable.

Description

Technical field [0001] The present invention relates to the field of aerodynamics, in particular to a control method and control device of a tilt rotor aircraft. Background technique [0002] In related technologies, fixed-wing aircraft and rotary-wing aircraft are two representatives of aircraft with different structures, and their development has attracted great attention from countries all over the world. Fixed-wing aircraft has the advantages of long range, low noise, and fast flying speed, but it is greatly affected by the take-off and landing environment and cannot hover in the air. Rotorcraft can achieve functions such as vertical take-off and landing, low-altitude and low-speed flight, and hovering in the air, but due to its own structural limitations, it has low load capacity, high noise, and short range. [0003] Later, the tiltrotor was proposed. The tiltrotor combines the vertical take-off and landing capability of a rotorcraft and the fast flying capability of a fixed...

Claims

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Application Information

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IPC IPC(8): G05B13/04
CPCG05B13/041
Inventor 白勍王国辉杨峥蒋本忠
Owner SHENYANG SHANGBO ZHITUO TECH CO LTD
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