Looking for breakthrough ideas for innovation challenges? Try Patsnap Eureka!

Method for constructing virtual test environment of environment control system software

A control system and virtual testing technology, applied in software testing/debugging, error detection/correction, instrumentation, etc., which can solve the problem of delaying the test plan and software product installation plan on time, and unable to test another version of ECS software at the same time. , delay the test plan software product installation plan on time and other issues, to achieve the effect of saving money

Inactive Publication Date: 2018-05-29
XIAN AIRCRAFT DESIGN INST OF AVIATION IND OF CHINA
View PDF4 Cites 5 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0010] f) Or, it often occurs that the only set of real hardware environment is developing and verifying the function of a certain version of ECS software, and the other version of ECS software cannot be tested at the same time, which delays the testing plan and software product installation plan on time;
[0011] g) Or, the only physical verification platform in the laboratory is in the state of troubleshooting airborne equipment in the field, and the ECS software test cannot be carried out at the same time, which delays the test plan and software product installation plan on time;

Method used

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
View more

Image

Smart Image Click on the blue labels to locate them in the text.
Viewing Examples
Smart Image
  • Method for constructing virtual test environment of environment control system software
  • Method for constructing virtual test environment of environment control system software
  • Method for constructing virtual test environment of environment control system software

Examples

Experimental program
Comparison scheme
Effect test

Embodiment Construction

[0042] In order to make the objectives, technical solutions and advantages of the present invention clearer, the technical solutions in the embodiments of the present invention will be described in more detail below in conjunction with the drawings in the embodiments of the present invention. In the drawings, the same or similar reference numerals denote the same or similar elements or elements having the same or similar functions throughout. The described embodiments are some, but not all, embodiments of the invention. The embodiments described below by referring to the figures are exemplary and are intended to explain the present invention and should not be construed as limiting the present invention. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without creative efforts fall within the protection scope of the present invention. Embodiments of the present invention will be described in detail below ...

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to View More

PUM

No PUM Login to View More

Abstract

The invention discloses a method for constructing a virtual test environment of environment control system software and belongs to the technical field of airborne system software testing. The method comprises the steps that first, comprehensive airborne electronic system network configuration containing an environment control system is constructed, and an interface associated with the environmentcontrol system is constructed; second, a virtual target machine associated with the environment control system is constructed, an embedded operating system is formed, a simulation control and displaymodule is constructed according to the network configuration, and a peripheral device model base is constructed; third, fault models of all systems are established, and a dynamic link library is developed to form an interface associated with the environment control system and the embedded operating system; and last, an auxiliary test tool is integrated and used for performing black-box and white-box testing on the environment control system software. Through the method, in the virtual test environment or system, environment control system airborne software configuration item testing can be completed independently and sufficiently without the influence of a real running environment of a flight management system.

Description

technical field [0001] The invention belongs to the technical field of airborne system software testing, in particular to a method for constructing a virtual testing environment for environment control system software. Background technique [0002] Integrated avionics system software and hardware integrated design technology has been widely used in various types of modern military and civilian aircraft. The environmental control system software (ECS software) realizes the centralized maintenance and management functions of each component system of the aircraft. [0003] At present, the R&D mode of environmental control system software (ECS software) starts with the overall or outline design of the software, and then starts the hardware equipment to reach the delivery status, and then the software R&D and testing personnel carry out the software design and development and unit component testing, and the software Hardware system integration testing and validation. [0004] Si...

Claims

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to View More

Application Information

Patent Timeline
no application Login to View More
Patent Type & Authority Applications(China)
IPC IPC(8): G06F11/36
CPCG06F11/3664G06F11/3696
Inventor 钱向农
Owner XIAN AIRCRAFT DESIGN INST OF AVIATION IND OF CHINA
Who we serve
  • R&D Engineer
  • R&D Manager
  • IP Professional
Why Patsnap Eureka
  • Industry Leading Data Capabilities
  • Powerful AI technology
  • Patent DNA Extraction
Social media
Patsnap Eureka Blog
Learn More
PatSnap group products