A System Dynamics Evaluation Model of Avionic Fuel Control System
- DOI
- 10.2991/meic-14.2014.124How to use a DOI?
- Keywords
- Avionics Fuel Control System; Aircraft; System dynamics; Vensim; Modeling and Evaluating
- Abstract
Avionics fuel control system, which is applied for delivering fuel to an engine in modern aircraft system, is difficult to study, design, and implement due to the high-security measures and the need for standard certification.To evaluate the complex dynamics involved in implementing fuel regulating for aircraft fuel system, a quantifiable evaluation model for avionics fuel control system based on system dynamics theory is developed in this paper. Firstly, the speed and flow regulation process is briefly introduced in an avionics fuel control system. Then, based on these operation principles, the analytic relations among the system state variables are provided, which come into being the system dynamics evaluation model. According to these analytic relations, the evalutation model is realized and simulated using Vensim tool. The simulation result shows that this model can be used efficiently in modeling and evaluating of avionic fuel control system for its clear causality, suitable complexity, and exact describe characteristics.
- Copyright
- © 2014, the Authors. Published by Atlantis Press.
- Open Access
- This is an open access article distributed under the CC BY-NC license (http://creativecommons.org/licenses/by-nc/4.0/).
Cite this article
TY - CONF AU - Zhen Zhao AU - Yigang Sun AU - Dexin Zhou AU - Hao Li PY - 2014/11 DA - 2014/11 TI - A System Dynamics Evaluation Model of Avionic Fuel Control System BT - Proceedings of the 2014 International Conference on Mechatronics, Electronic, Industrial and Control Engineering PB - Atlantis Press SP - 552 EP - 555 SN - 2352-5401 UR - https://doi.org/10.2991/meic-14.2014.124 DO - 10.2991/meic-14.2014.124 ID - Zhao2014/11 ER -