Research on Uncertainty Measurement Method of Aircraft HWIL System

Authors

Huapin Geng, 1. Beijing Electro-Mechanical Engineering Institute, Beijing 100074, China; ;
Jiahui Tong, 2. Science and Technology on Complex System Control and Intelligent Agent Cooperation Laboratory, Beijing 100074, China; ;
Hongtao Ma, 3. Beijing Xinghang Mechanical and Electrical Equipment Co., Ltd, Beijing 100074, China;

Abstract

Abstract: Uncertainty is the inherent attribute of simulation system, causing the expected results inconformity with the real results, even influencing the robustness and reliability of system. Based on the analysis of the system uncertainty characteristics, the analysis framework of HWIL system uncertainty measurement is proposed. Three kinds of the uncertainty measurement methods based on the uncertainty type and the compound and weighting are researched on aircraft HWIL System. The typical uncertainty measurement methods are applied based on some aircraft HWIL system and the result proves that the method is efficient.

Recommended Citation

Geng, Huapin; Tong, Jiahui; and Ma, Hongtao (2019) "Research on Uncertainty Measurement Method of Aircraft HWIL System," Journal of System Simulation: Vol. 31: Iss. 12, Article 14.
DOI: 10.16182/j.issn1004731x.joss.19-FZ0385
Available at: https://dc-china-simulation.researchcommons.org/journal/vol31/iss12/14

First Page

2671

Revised Date

2019-07-30

DOI Link

https://doi.org/10.16182/j.issn1004731x.joss.19-FZ0385

Last Page

2677

CLC

TP391.9

Recommended Citation

Geng Huapin, Tong Jiahui, Ma Hongtao. Research on Uncertainty Measurement Method of Aircraft HWIL System[J]. Journal of System Simulation, 2019, 31(12): 2671-2677.

DOI

10.16182/j.issn1004731x.joss.19-FZ0385