Journal of System Simulation
Abstract
Abstract: In the past, there were some problems in the software design for the flight simulation avionics system such as the decentralized structure and the low degree of modularization. Aiming at these problems, a hierarchical, modular integrated avionics system is constructed. The logic part dispersed in each function module is independent to form the integrated logic module. Each task function module and its sub module are responsible for the calculation of the relevant task function algorithm. Modular design is carried out in a deeper level. By dataflow analysis, each module in this design has strong cohesion and weak coupling and strong independence. The whole design structure is reasonable; the program is understandable and readable; and the software is reliable and maintainable.
Recommended Citation
Zhao, Mingbo; Long, Pan; Jiang, Longwei; Gang, Wang; and Zhao, Guangxing
(2019)
"Modular Design Method of Integrated Avionics Simulation System,"
Journal of System Simulation: Vol. 31:
Iss.
2, Article 21.
DOI: 10.16182/j.issn1004731x.joss.17-0079
Available at:
https://dc-china-simulation.researchcommons.org/journal/vol31/iss2/21
First Page
339
Revised Date
2017-04-06
DOI Link
https://doi.org/10.16182/j.issn1004731x.joss.17-0079
Last Page
345
CLC
TP391.9
Recommended Citation
Zhao Mingbo, Pan Long, Jiang Longwei, Wang Gang, Zhao Guangxing. Modular Design Method of Integrated Avionics Simulation System[J]. Journal of System Simulation, 2019, 31(2): 339-345.
DOI
10.16182/j.issn1004731x.joss.17-0079
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