CN117434921A - Hardware testing system and method of flight simulation trainer - Google Patents

Abstract

The invention discloses a hardware test system of a flight simulation trainer, which comprises a real-time operation module, a calibration module, a downloading module, an operation parameter acquisition module, a detection module, an abnormal data extraction module, a positioning module and a communication module, wherein the real-time operation module, the calibration module and the downloading module are respectively connected with the flight simulation trainer, the real-time operation module is connected with the operation parameter acquisition module, the operation parameter acquisition module is connected with the detection module, the detection module is connected with the abnormal data extraction module, the abnormal data extraction module is connected with the positioning module, the downloading module, the calibration module and the abnormal data extraction module are respectively connected with the communication module, and the communication module is connected with equipment of staff. The invention constructs a testing system integrating configuration, calibration and testing hardware, realizes visual, accurate and effective testing, saves time and improves testing efficiency.

Description

Hardware testing system and method of flight simulation trainer

Technical Field

The invention relates to the technical field of flight simulation trainer testing, in particular to a hardware testing system and a testing method of a flight simulation trainer.

Background

Flight simulators (Flight simulators), which are devices used to simulate the Flight of an aircraft, such as aircraft, missiles, satellites, spacecraft, etc., are known in a broad sense as Flight simulators, which are devices that reproduce the environment of the aircraft and the air and are capable of operating, in a narrow sense, as devices that simulate the Flight of an aircraft and that are relatively complex in structure and function. A flight simulator is referred to as a flight simulator if it is relatively simple in structure and has little functionality.

At present, when the existing flight simulation trainer tests hardware, the hardware is tested by manually analyzing data according to a communication protocol and receiving and sending data through a network debugging assistant, so that the manual test is difficult and easy to make mistakes.

Therefore, a hardware testing system of a flight simulation trainer and a testing method thereof are provided for solving the problems.

Disclosure of Invention

The invention aims to provide a hardware test system of a flight simulation trainer, which comprises a real-time operation module, a calibration module, a downloading module, an operation parameter acquisition module, a detection module, an abnormal data extraction module, a positioning module and a communication module, wherein the real-time operation module, the calibration module and the downloading module are respectively connected with the flight simulation trainer, the real-time operation module is connected with the operation parameter acquisition module, the operation parameter acquisition module is connected with the detection module, the detection module is connected with the abnormal data extraction module, the abnormal data extraction module is connected with the positioning module, the downloading module, the calibration module and the abnormal data extraction module are respectively connected with the communication module, and the communication module is connected with equipment of staff.

Preferably, a method for testing a hardware testing system of a flight simulation trainer, the testing steps include:

step one: if the device is the primary test device, calibrating a potentiometer of the flight simulation trainer through a calibration module, and downloading parameters of the flight simulation trainer in advance through a downloading module; if the test is not the primary test equipment, the test is carried out under the condition that the fault is required to be removed, the operation of the step two is directly carried out:

step two: when any one of the switch buttons is pressed, the parameters regulated by the button and the real-time regulation parameters of the corresponding hardware of the button are obtained in real time through an operation parameter obtaining module;

step three: the method comprises the steps that the obtained button adjusting parameters and hardware state parameters are detected through a detection module, a standard threshold range of each hardware parameter is preset in the detection module, and data exceeding the threshold range is extracted through an abnormal data extraction module;

step four: the positioning module is used for positioning each piece of abnormal data, and transmitting the positioning information and the abnormal data information to equipment of staff through the communication module, so that the staff can overhaul the fault position conveniently;

step five: judging whether hardware configuration parameters or calibration potentiometer data need to be downloaded again according to the fault problem obtained in the step four.

Compared with the prior art, the invention has the following beneficial effects:

according to the invention, abnormal data is extracted and the abnormal position is positioned through the cooperation of the real-time operation module, the operation parameter acquisition module, the detection module, the abnormal data extraction module, the positioning module and the communication module, so that the maintenance of staff is facilitated; the hardware configuration parameters can be downloaded through the downloading module by one key, the signal value of the potentiometer can be converted into an ideal value through the calibrating module, a testing system integrating configuration, calibration and testing hardware is built, visual, accurate and effective testing is realized, time is saved, and testing efficiency is improved.

Drawings

FIG. 1 is a schematic diagram of the system connection structure of the present invention;

FIG. 2 is an internal schematic view of the detection module of the present invention;

FIG. 3 is a schematic diagram of the method steps of the present invention.

Detailed Description

The following description of the embodiments of the present invention will be made clearly and completely with reference to the accompanying drawings, in which it is apparent that the embodiments described are only some embodiments of the present invention, but not all embodiments. All other embodiments, which can be made by those skilled in the art based on the embodiments of the invention without making any inventive effort, are intended to be within the scope of the invention.

As shown in fig. 1 and 2, the hardware testing system of the flight simulation trainer provided by the invention comprises a real-time operation module, a calibration module, a downloading module, an operation parameter acquisition module, a detection module, an abnormal data extraction module, a positioning module and a communication module, wherein the detection module respectively comprises a hardware state detection unit and a panel detection unit, the hardware state detection unit is used for detecting whether hardware works normally, and the panel detection unit comprises five parts, namely communication detection, switch detection, potentiometer detection, encoder detection and instrument signal detection;

the real-time operation module, the calibration module and the downloading module are respectively connected with the flight simulation trainer, the real-time operation module is connected with the operation parameter acquisition module, the operation parameter acquisition module is connected with the detection module, the detection module is connected with the abnormal data extraction module, the abnormal data extraction module is connected with the positioning module, the downloading module, the calibration module and the abnormal data extraction module are respectively connected with the communication module, and the communication module is connected with equipment of staff.

Example 1:

as shown in fig. 3, if the test device is the primary test device:

step one: potentiometer calibration is carried out on the flight simulation trainer through a calibration module, and parameter downloading is carried out on the flight simulation trainer in advance through a downloading module

Step two: when any one of the switch buttons is pressed, the parameters regulated by the button and the real-time regulation parameters of the corresponding hardware of the button are obtained in real time through an operation parameter obtaining module;

step three: the method comprises the steps that the obtained button adjusting parameters and hardware state parameters are detected through a detection module, a standard threshold range of each hardware parameter is preset in the detection module, and data exceeding the threshold range is extracted through an abnormal data extraction module;

step four: the positioning module is used for positioning each piece of abnormal data, and transmitting the positioning information and the abnormal data information to equipment of staff through the communication module, so that the staff can overhaul the fault position conveniently.

Example 2:

if the test equipment is not primary test equipment, the test is carried out under the condition that the fault needs to be removed:

step one: when any one of the switch buttons is pressed, the parameters regulated by the button and the real-time regulation parameters of the corresponding hardware of the button are obtained in real time through an operation parameter obtaining module;

step two: the method comprises the steps that the obtained button adjusting parameters and hardware state parameters are detected through a detection module, a standard threshold range of each hardware parameter is preset in the detection module, and data exceeding the threshold range is extracted through an abnormal data extraction module;

step three: the positioning module is used for positioning each piece of abnormal data, and transmitting the positioning information and the abnormal data information to equipment of staff through the communication module, so that the staff can overhaul the fault position conveniently;

step four: judging whether hardware configuration parameters or calibration potentiometer data need to be downloaded again according to the fault problem obtained in the steps.

In the description of the present invention, it should be noted that, unless explicitly specified and limited otherwise, the terms "mounted," "provided," "connected," and the like are to be construed broadly, and may be fixedly connected, detachably connected, or integrally connected, for example; can be mechanically or electrically connected; can be directly connected or indirectly connected through an intermediate medium, and can be communication between two elements. The specific meaning of the above terms in the present invention will be understood in specific cases by those of ordinary skill in the art.

Claims (7)

1. A hardware testing system of a flight simulation trainer, which is characterized in that: the device comprises a real-time operation module, a calibration module, a downloading module, an operation parameter acquisition module, a detection module, an abnormal data extraction module, a positioning module and a communication module, wherein the real-time operation module, the calibration module and the downloading module are respectively connected with a flight simulation trainer, the real-time operation module is connected with the operation parameter acquisition module, the operation parameter acquisition module is connected with the detection module, the detection module is connected with the abnormal data extraction module, the abnormal data extraction module is connected with the positioning module, the downloading module, the calibration module and the abnormal data extraction module are respectively connected with the communication module, and the communication module is connected with equipment of staff.

2. A hardware testing system for a flight simulation trainer according to claim 1, wherein: the detection module comprises a hardware state detection unit and a panel detection unit respectively.

3. A hardware testing system for a flight simulation trainer according to claim 1, wherein: the hardware state detection unit is used for detecting whether the hardware works normally or not.

4. A hardware testing system for a flight simulation trainer according to claim 1, wherein: the panel detection unit comprises five parts, namely communication detection, switch detection, potentiometer detection, encoder detection and instrument signal detection.

5. A hardware testing system for a flight simulation trainer according to claim 1, wherein: the calibration module is used for converting the signal value into an ideal value by the potentiometer.

6. A hardware testing system for a flight simulation trainer according to claim 1, wherein: the downloading module is used for downloading hardware configuration parameters by one key.

7. The method for testing a hardware testing system of a flight simulation trainer according to claim 1, wherein: the testing steps comprise:

step one: if the device is the primary test device, calibrating a potentiometer of the flight simulation trainer through a calibration module, and downloading parameters of the flight simulation trainer in advance through a downloading module; if the test is not the primary test equipment, the test is carried out under the condition that the fault is required to be removed, the operation of the step two is directly carried out:

step two: when any one of the switch buttons is pressed, the parameters regulated by the button and the real-time regulation parameters of the corresponding hardware of the button are obtained in real time through an operation parameter obtaining module;

step three: the method comprises the steps that the obtained button adjusting parameters and hardware state parameters are detected through a detection module, a standard threshold range of each hardware parameter is preset in the detection module, and data exceeding the threshold range is extracted through an abnormal data extraction module;

step four: the positioning module is used for positioning each piece of abnormal data, and transmitting the positioning information and the abnormal data information to equipment of staff through the communication module, so that the staff can overhaul the fault position conveniently;

step five: judging whether hardware configuration parameters or calibration potentiometer data need to be downloaded again according to the fault problem obtained in the step four.