Design of Hardware-in-the-loop Simulation Platform in Propulsion Control Systems of Aero-Engine

DOI

10.2991/emcm-16.2017.67How to use a DOI?

Keywords

Aero-engine; Hardware-in-the-loop; System simulation; SPI communication; CRC verification

Abstract

The performance of the electronic controller is of significance to the development of turbofan engine with afterburner. To verify the feasibility of the control algorithm and the design scheme of hardware and software of the controller, the embedded computer based on PC104 architecture was used as the electronic controller, the C8051F320, ADuC7020, and ACEX1K50 microprocessors were adopted as the signal interface regulate box of the engine model computer. The C and VHDL language were employed to develop the system, a simulation experimental platform of hardware-in-the-loop was thus designed. Simulation results of hardware-in-the-loop show that the controlled parameter of the engine tends to the final expected value, and the fidelity of the signal transmission of the physical quantities between the electronic controller and the engine digital model is favorable.

Copyright

© 2017, 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/).

Download article (PDF)

TY  - CONF
AU  - Bei Yang
AU  - Xiaowu Ding
PY  - 2017/02
DA  - 2017/02
TI  - Design of Hardware-in-the-loop Simulation Platform in Propulsion Control Systems of Aero-Engine
BT  - Proceedings of the 2016 7th International Conference on Education, Management, Computer and Medicine (EMCM 2016)
PB  - Atlantis Press
SN  - 2352-538X
UR  - https://doi.org/10.2991/emcm-16.2017.67
DO  - 10.2991/emcm-16.2017.67
ID  - Yang2017/02
ER  -