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Flight control movable surface deflection angle determination method and system

A technology of deflection angle and determination method, which is applied in aircraft component testing, image analysis, instruments, etc., can solve the problems of poor measurement accuracy, difficulty in measurement, installation error, etc., and achieve good applicability

Pending Publication Date: 2022-07-19
SHANGHAI AIRCRAFT MFG
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

However, manual measurement has the defects of poor accuracy and low measurement efficiency; the structure of mechanical measurement is complex, which may introduce installation errors, and it is necessary to read the angle value near each active surface; The measurement accuracy of the rotation angle of the heading direction is poor, and it is difficult to measure the translational data of the flaps and slats, which are both rotating and translational.

Method used

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  • Flight control movable surface deflection angle determination method and system
  • Flight control movable surface deflection angle determination method and system
  • Flight control movable surface deflection angle determination method and system

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Embodiment Construction

[0029] The present application will be further described in detail below with reference to the accompanying drawings and embodiments. It should be understood that the specific embodiments described herein are only used to explain the present application, but not to limit the present application. In addition, it should be noted that, for the convenience of description, the drawings only show some but not all the structures related to the present application.

[0030] In addition, in the embodiments of the present application, words such as "optionally" or "exemplarily" are used to represent examples, illustrations, or illustrations. Any embodiments or designs described in the embodiments of the present application as "optionally" or "exemplarily" should not be construed as preferred or advantageous over other embodiments or designs. Rather, the use of words such as "optionally" or "exemplarily" is intended to present the related concepts in a specific manner.

[0031] figur...

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Abstract

The invention discloses a flight control active surface deflection angle determination method and system. The method comprises the steps of obtaining three-dimensional coordinates and mark point classification information of mark points on an active surface at the current moment; determining an activity surface type according to the mark point classification information; determining a corresponding calculation scheme according to the activity surface type; and according to the calculation scheme and the three-dimensional coordinates of the mark points, determining the deflection angle of the movable surface rotating from the reference moment to the current moment. By means of the designed mode, the rotation angle of the movable face can be determined according to the mark points on the movable faces of different types, and the method can be suitable for the special situation that the movable face is provided with a plurality of mark points, one mark point or two mark points and has good applicability.

Description

technical field [0001] The embodiments of the present application relate to the field of civil aircraft testing, and in particular, to a method and system for determining a deflection angle of a flight control active surface. Background technique [0002] During the flight of the aircraft, the attitude of the aircraft is usually controlled by the deflection of the active surfaces of the wings and tail. In order to verify whether the deflection of these active surfaces meets the requirements, it is often necessary to measure the deflection angles of these active surfaces, such as figure 1 Shown is a schematic diagram of the active surface of the aircraft. [0003] The traditional measurement methods of the deflection angle of the movable surface mainly include manual measurement, mechanical measurement and microelectromechanical systems (Microelectro Mechanical Systems, MEMS) gyro ritual measurement. Among them, the manual measurement is to measure the straight-line distance...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64F5/60G06T7/73G06T7/50G06K9/62G06F21/31
CPCB64F5/60G06T7/73G06T7/50G06F21/31G06F18/24
Inventor 段曙凯李徐辉吴熙童彦沈乐刚魏士皓杨达勇
Owner SHANGHAI AIRCRAFT MFG
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