Airplane full static pressure test system based on adaptive PID method and method

Abstract

The invention relates to an airplane full static pressure test system based on an adaptive PID method and a method. According to the method, a power source starts power supply, self check is carried out; if correct, an analysis step of an instruction is carried out; if not correct, re-input of the instruction is carried out; a core module is controlled for converting and analyzing the instruction; the instruction is actuated; whether an emergency stop instruction is emitted is determined; if yes, the program is ended; if not, acquisition of pressure values of a sensor II and a sensor IV starts; values of the sensor II and the sensor IV are continuously acquired; the core module is controlled for checking whether a target value is reached; if yes, the progress is over; if not, the instruction is re-actuated. Through the method, a precise and reliable pressure source can be provided by the system for an airplane according to setting of an operator, real-time response can be carried out according to different demands of a test process, the airplane can be protected under emergent situations such as shedding of a pressure connector, and test tasks prescribed in an airplane manual can be accomplished according to demands of the airplane manual.

Description

technical field [0001] The invention belongs to the field of automatic testing, in particular to an aircraft full static pressure testing system and method based on an adaptive PID method. Background technique [0002] The full static pressure test system is used in the infield maintenance and outfield maintenance where the full static pressure test of the aircraft is required. The system provides corresponding air pressure sources for the aircraft full static pressure system according to the operating instructions of the tester. At present, the aircraft full static pressure test system has high purchase cost, high maintenance cost, and long maintenance cycle, which brings inconvenience to the normal operation of the airline company, and even brings certain risks to flight safety due to the change of accuracy and air tightness caused by long-distance transportation. influences. In addition, the existing tester mainly relies on the ball valve for pressure change operation, w...

AI Technical Summary

Problems solved by technology

[0003] The purpose of the present invention is to solve the existing technical problems, aiming at the inconvenience in the use and maintenance of the full static pressure test equipment of airlines, and to solve the current situation that the test requirements of the full static pressure system are difficult to meet, and to provide a low cost, simple structure, An aircraft full static pressure test system and method based on an adaptive PID method capable of rapid testing, convenient calibration and maintenance, convenient access to aircraft systems, and meeting the test requirements of airline maintenance manuals

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