| 冲压发动机控制系统的半实物仿真试验研究 |
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| 引用本文： | 徐中节,尤裕荣,逯婉若,吴宝元.冲压发动机控制系统的半实物仿真试验研究[J].火箭推进,2010,36(1):63-66. |
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| 作者姓名： | 徐中节 尤裕荣 逯婉若 吴宝元 |
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| 作者单位： | 西安航天动力研究所,陕西,西安,710100 |
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| 摘 要： | 将燃油调节器、电子控制器以实物形式接入半实物仿真试验系统,将控制回路另外部分包括对象发动机和导弹的动态特性在数字仿真器上实现。数字仿真器通过输入输出接口与冲压发动机的控制器进行联接,从而搭建了冲压发动机控制系统的半实物仿真试验平台。通过一系列半实物仿真试验表明,构建的平台可以实现考核控制系统设计的目的。
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| 关 键 词： | 控制系统半实物仿真数字电子控制器 |
Research on hardware-in-loop simulation tests of a ramjet engine control system |
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| Xu Zhongjie,You Yurong,Lu Wanruo,Wu Baoyuan.Research on hardware-in-loop simulation tests of a ramjet engine control system[J].Journal of Rocket Propulsion,2010,36(1):63-66. |
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| Authors: | Xu Zhongjie You Yurong Lu Wanruo Wu Baoyuan |
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| Institution: | (Xi＇an Aerospace Propulsion Institute, Xi＇an 710100,China) |
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| 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. |
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| Keywords: | control system hardware-in-loop simulation digital electronic controller |
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