| 战斗机综合设计仿真系统中的飞控系统模型 |
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| 引用本文： | 刘艳,高正红,商重阳.战斗机综合设计仿真系统中的飞控系统模型[J].飞行力学,2006,24(4):22-25,29. |
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| 作者姓名： | 刘艳 高正红 商重阳 |
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| 作者单位： | 西北工业大学,航空学院,陕西,西安,710072 |
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| 摘 要： | 通过分析飞控系统各环节对飞机动态特性的影响及第三代战斗机控制律的特点,为战斗机综合设计仿真系统建立了飞控系统模型。该模型是能够反映飞控系统功能的简化模型。通过对飞控系统各项功能与特点的检验,对飞控系统简化模型进行了验证。验证结果表明,所建立的简化飞控系统模型能够满足战斗机综合设计仿真系统的需要。
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| 关 键 词： | 综合设计 仿真系统 飞控系统 简化模型 |
| 文章编号： | 1002-0853（2006）04-0022-04 |
| 收稿时间： | 2005-09-23 |
| 修稿时间： | 2005-09-232006-05-24 |
A Flight Control System Model of the Fighter Integrated Design Simulation System |
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| LIU Yan,GAO Zheng-hong,SHANG Chong-yang.A Flight Control System Model of the Fighter Integrated Design Simulation System[J].Flight Dynamics,2006,24(4):22-25,29. |
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| Authors: | LIU Yan GAO Zheng-hong SHANG Chong-yang |
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| Abstract: | By analyzing the effects of every part of a flight control system(FCS) on the dynamics of the aircraft,and the characteristics of the 3~(rd) generation fighter's FCS,the FCS of the fighter integrated design simulation system is modeled.Such model is a simplified model,which can indicate the characteristics and functions of the FCS.The simplified model is validated by verifying the main characteristics and functions of the FCS.The results indicate that the simplified model can satisfy the requirements of the fighter integrated design simulation system. |
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| Keywords: | integrated design simulation system flight control system simplified model |
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