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

A Hybrid Heterogeneous Simulation Platform for Civil Aircraft Flight Control System

A flight control system and simulation platform technology, applied in the field of civil aircraft flight control, can solve problems such as low level of simulation, unclear simulation interface, and inconspicuous model replacement function, and achieve the effect of improving differences

Active Publication Date: 2018-06-29
BEIJING AERONAUTIC SCI & TECH RES INST OF COMAC +1
View PDF5 Cites 0 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

In the common civil aircraft flight control system simulation platforms, there are mainly the Iron Bird platform composed of real parts, or the flight control system model platform based on a single computer for modeling. For the traditional flight control Iron Bird platform, due to the existence of multiple versions The upgrade of flight control software and hardware, the evaluation of configuration differences involved, the analysis of safety impact, the recurrence of system function faults, and the application of multi-system software integration are problems to be solved urgently. For the flight control system model of a single computer, due to the simulation interface It is not clear, the degree of simulation is not high, it has been in the model development stage, and it cannot replace the Iron Bird test bench, and its model replacement function is not outstanding

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
  • A Hybrid Heterogeneous Simulation Platform for Civil Aircraft Flight Control System
  • A Hybrid Heterogeneous Simulation Platform for Civil Aircraft Flight Control System
  • A Hybrid Heterogeneous Simulation Platform for Civil Aircraft Flight Control System

Examples

Experimental program
Comparison scheme
Effect test

Embodiment Construction

[0032] In order to make the object, technical solution and advantages of the present invention clearer, the present invention will be further described in detail below in conjunction with the accompanying drawings and embodiments. It should be understood that the specific embodiments described here are only used to explain the present invention, not to limit the present invention. On the contrary, the invention covers any alternatives, modifications, equivalent methods and schemes within the spirit and scope of the invention as defined by the claims. Further, in order to make the public have a better understanding of the present invention, some specific details are described in detail in the detailed description of the present invention below. The present invention can be fully understood by those skilled in the art without the description of these detailed parts.

[0033] The present invention will be further described below in conjunction with the accompanying drawings and ...

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 provides a civil airplane flight control system mixing heterogeneous simulation platform. The platform employs three flight control module units and four actuator control electronic units for effectively supporting different frameworks in a flight control system 12, 8 actuating strategies of a flight control actuator, and balance and assessment of mixing heterogeneous integration simulation in a flight control system 96; a security analysis in theory is conducted according to the obtained test difference data; and the analysis is stored in an integrated control unit to construct a security analysis database. Each accessed true member and model are synchronized according to heartbeat synchronization. Fault is determined if time isn't synchronized, in this way, fault reproduction and analysis can be conducted; interface analysis and contrast among each accessed true members and the model are conducted according to a general bus management unit and an interface simulation unit; and difference between the model and a true member is improved by improving model simulation degree according to history data and test data.

Description

technical field [0001] The invention belongs to the field of civil aircraft flight control, and in particular relates to a hybrid heterogeneous simulation platform for a civil aircraft flight control system. Background technique [0002] The hybrid heterogeneous simulation platform for civil aircraft flight control system is a simulation test platform for civil aircraft, which is mainly used for the simulation development of flight control system model, the test and verification of the real part access system, and the mixed heterogeneity of the model and the real part joint simulation. In the common civil aircraft flight control system simulation platforms, there are mainly the Iron Bird platform composed of real parts, or the flight control system model platform based on a single computer for modeling. For the traditional flight control Iron Bird platform, due to the existence of multiple versions The upgrade of flight control software and hardware, the evaluation of confi...

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 Patents(China)
IPC IPC(8): G06F17/50G05B23/02
CPCG05B23/02G06F30/15G06F30/367
Inventor 李喜玉熊斯白志强
Owner BEIJING AERONAUTIC SCI & TECH RES INST OF COMAC
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