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Aviation simulation flight ground level meter based on can bus control

A CAN bus and flight simulation technology, applied in the field of aviation simulation, can solve the problems of inability to configure independent functional units, large structural size, slow response speed, etc., and achieve the effect of compact structure, excellent response speed and high reliability

Active Publication Date: 2022-03-29
SHANGHAI AVIATION ELECTRIC
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] The horizon meter is an aircraft flight attitude indicating device. Currently, the horizon meter used for flight simulation generally uses an industrial stepping motor as a power source, which has a large structure size, slow response speed, large noise, and cannot be independently configured as an independent functional unit, etc. question

Method used

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  • Aviation simulation flight ground level meter based on can bus control
  • Aviation simulation flight ground level meter based on can bus control
  • Aviation simulation flight ground level meter based on can bus control

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Embodiment Construction

[0028] The present invention will be further described in detail below in conjunction with the accompanying drawings and embodiments.

[0029] Such as figure 1 , figure 2 and image 3 Shown is a schematic diagram of the structure of the aviation flight simulation horizon table based on CAN bus control.

[0030] The aviation analog flight ground level meter based on CAN bus control includes protective glass, pitch angle rotation mechanism, horizontal angle rotation mechanism, fixed mounting plate, drive control printed circuit board, control printed circuit board bracket and a case for encapsulating the above-mentioned components and back cover. Wherein, the protective glass is installed on the watch case, and is located above the horizontal angle rotation mechanism to play a protective role. The pitch angle rotation mechanism is embedded in the horizontal angle rotation mechanism, and the drive control printed circuit board is arranged on the fixed installation board thro...

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Abstract

The invention belongs to aviation simulation technology, and specifically provides an aviation simulation flight horizon meter based on CAN bus control. The aviation simulation flight horizon table based on CAN bus control includes a protective glass, a pitch angle rotation mechanism, a horizontal angle rotation mechanism, a fixed mounting plate, a drive control printed circuit board, a control printed circuit board bracket, and a package for packaging the above-mentioned components. The watch case and the back cover, wherein the protective glass is installed on the watch case and is located above the horizontal angle rotation mechanism, the pitch angle rotation mechanism is embedded in the horizontal angle rotation mechanism, and the drive control printed circuit board passes through the control printed circuit board The bracket is arranged on the fixed mounting plate. The aviation simulation flight horizon table based on CAN bus provided by the invention has the following advantages: compact structure, high data transmission rate, fast response speed, high reliability, uniform luminescence, good display effect, as a whole functional unit, independent configuration, can Meet the application requirements of different models of simulated aircraft.

Description

technical field [0001] The invention belongs to the aviation simulation technology, and in particular relates to an aviation simulation flight level indicator based on CAN bus control, which is especially suitable for the simulation indicating device of the aircraft flight attitude of the aviation simulation flight training device. Background technique [0002] Simulated flight simulators are widely used in aircraft driving training, which can greatly improve the flight safety and training effect of aircraft driving training, and greatly reduce the cost of real flight training. In order to ensure the training effect, the ground flight simulation trainer needs to be as consistent as possible with the state of the real aircraft flying in the air, and because the instruments on the real aircraft basically use physical quantities such as air pressure, altitude, geomagnetism, rotation, and acceleration as equipment. The power source or signal source is directly driven, so to ensu...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G09B9/20
CPCG09B9/20
Inventor 曾伟明张洪建王猛
Owner SHANGHAI AVIATION ELECTRIC
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