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Configurable display and control method and device for aircraft launch process

An aircraft and process technology, applied in instruments, general control systems, electrical testing/monitoring, etc., can solve problems such as errors, and achieve the effect that errors are less likely to occur, and the adjustment method is simple and feasible

Active Publication Date: 2017-02-22
BEIJING INST OF ELECTRONICS SYST ENG
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] The purpose of the present invention is to solve the problem that the existing method of adjusting the launch process of the aircraft is prone to errors. The present invention provides a display and control method and device with configurable launch process of the aircraft

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  • Configurable display and control method and device for aircraft launch process

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specific Embodiment approach 1

[0040] Specific implementation mode one: combine figure 1 Describe this embodiment, the display and control method of the configurable aircraft launch process described in this embodiment, the method includes the following steps:

[0041] Create a required test process according to the aircraft launch process, adjust the test process, and generate a launch process configuration file;

[0042] A step of saving the process information in the generated process configuration file;

[0043] Read the process configuration file, call the corresponding command in the command set according to the process information in the process configuration file, and display the process information.

[0044] Said creation of the required test process according to the aircraft launch process can adjust the test process, and the steps of generating the launch process configuration file include:

[0045] Steps to define the structure;

[0046] The structure includes a command structure, a process s...

specific Embodiment approach 2

[0057] In this step, all the test command information saved in the launch process configuration file is sequentially displayed as each test command operation button. And to achieve interface, user-friendly operation. Specific implementation mode 2: This implementation mode is a display and control device with configurable aircraft launch process.

[0058] The device includes the following modules:

[0059] Create the required test process according to the aircraft launch process, adjust the test process, and generate a module for the launch process configuration file;

[0060] A module that saves the process information in the generated process configuration file;

[0061] Read the process configuration file, call the corresponding command in the command set according to the process information in the process configuration file, and display the process information.

[0062] According to the creation of the required test process according to the aircraft launch process, the ...

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Abstract

A display control method and a display control device for aircraft launching process configuration relate to the field of aircraft launching process control, and are provided to solve the problem that the existing method for adjusting the launching process of an aircraft is error-prone. The method comprises the following steps: creating a required test process according to an aircraft launching process and adjusting the test process to generate a launching process configuration file; storing process information in the generated process configuration file; and reading the process configuration file, calling a corresponding command in a command set according to the process information of the process configuration file, and displaying the process information. The display control method and the display control device of the invention are used for aircraft launching process control.

Description

technical field [0001] The invention relates to the field of aircraft launch process control. Background technique [0002] In the process of aircraft development, different test stages have different requirements for the launch control process. The design of the traditional software launch control process is fixed, and the adjustment of the launch process mainly depends on modifying the software code and upgrading the software to adjust the required launch control process. In this case, it is very easy to generate unpredictable errors in the process of code modification. Therefore, there are higher requirements for software programming. With the gradual increase in the reliability and security requirements of the weapon system, it is necessary to carry out a special design for the reliability and flexibility of the software. Contents of the invention [0003] The purpose of the present invention is to solve the problem that the existing method for adjusting the launch ...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G05B23/02
CPCG05B23/0259
Inventor 田福强王玉姣程鹏邓昕才
Owner BEIJING INST OF ELECTRONICS SYST ENG
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