Flight simulation horizon based on CAN bus control

Abstract

The invention belongs to the technology of flight simulation, and particularly provides a flight simulation horizon based on CAN bus control. The flight simulation horizon based on CAN bus control comprises protective glass, a pitch angle rotating mechanism, a horizontal angle rotating mechanism, a fixed mounting plate, a drive-controlled printed circuit board, a controlled printed circuit board support, a surface shell for packaging the above components and a rear cover, wherein the protective glass is arranged on the surface shell and is located above the horizontal angle rotating mechanism; the pitch angle rotating mechanism is embedded in the horizontal angle rotating mechanism; and the drive-controlled printed circuit board is arranged on the fixed mounting plate through the controlled printed circuit board support. The flight simulation horizon based on CAN bus control has the following advantages that the structure is compact; the data transmission rate is high; the response speed is quick; the reliability is high; light emission is uniform; the display effects are good; independent configuration as a function unit for the whole can be realized; and application requirements of simulation aircrafts with different models can be met.

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...

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

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