Airplane automatic control assembly test system
The invention belongs to the technical field of airplane automatic control component testing, and relates to an airplane automatic control component test system which comprises an industrial personal computer which is provided with a built-in airplane simulation model and can output airplane autothr...
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| Format: | Patent |
| Sprache: | chi ; eng |
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| Zusammenfassung: | The invention belongs to the technical field of airplane automatic control component testing, and relates to an airplane automatic control component test system which comprises an industrial personal computer which is provided with a built-in airplane simulation model and can output airplane autothrottle control instruction, an airplane accelerator control pull rod and engine main pump simulation device which is connected with the industrial personal computer, and an airplane automatic accelerator control assembly which is connected with the industrial personal computer, the airplane accelerator control pull rod and the engine main pump simulation device so as to control the airplane accelerator and engine main pump simulation device to act according to the airplane automatic accelerator control instruction; the industrial personal computer can receive feedback information of actions of the airplane accelerator control pull rod and engine main pump simulation device, solve an airplane simulation model and out |
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