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Research on hardware-in-loop simulation tests of a ramjet engine control system(PDF)

《火箭推进》[ISSN:1672-9374/CN:CN 61-1436/V]

Issue:
2010年01期
Page:
63-66
Research Field:
测控与试验
Publishing date:

Info

Title:
Research on hardware-in-loop simulation tests of a ramjet engine control system
Author(s):
Xu Zhongjie;  You Yurong;  Lu Wanruo;  Wu Baoyuan
Xi'an Aerospace Propulsion Institute, Xi'an 710100,China
Keywords:
-
PACS:
V439
DOI:
-
Abstract:
The experimental simulation system is composed of the digital electronic controller, fuel regulator and an integrative digital simulator while the mathematical models of ramjet engine and missile body are built integrally in the digital simulator. The simulator is connected with a real controller of a ramjet engine through the input and output interfaces. The results of hardware in the loop experiment show that the requirements of the testing of the control system are satisfied.

References:

[1]刘兴洲. 飞航导弹动力装置[M]. 北京：宇航出版社, 1992. [2]苏三买. 微型涡喷发动机数字控制实时半物理模拟试验系统[J]. 航空动力学报， 2001, 16(1): 93-96. [3]张世柽. 航空发动机设计手册 第15册[M]. 航空工业出版社, 2002. [4]陈万农. 航空发动机数控系统通用仿真和开发平台的构筑[J]. 燃气涡轮试验与研究, 2002, 15(3): 1-4. [5]程涛. 小型涡喷发动机数控调节器的半实物仿真[J]. 航空动力学报, 2004, 19(3): 383-386. [6]刘爱萍. 高推重比发动机全权限数字电子控制系统研究和半物理仿真试验验证[J]. 航空发动机, 2003, 29(1): 23-26.

Memo

Memo:
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Last Update: 1900-01-01