| 战机飞行仿真系统设计 |
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| 引用本文： | 曲志刚.战机飞行仿真系统设计[J].价值工程,2012,31(34):184-186. |
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| 作者姓名： | 曲志刚 |
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| 作者单位： | 海军航空工程学院青岛校区,青岛,266041 |
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| 摘 要： | 本文以F16飞机为例,详细介绍了飞机飞行仿真平台的设计方法,该方法可推广应用于其他飞机,可用于研究和仿真验证飞机飞行控制系统的控制性能。
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| 关 键 词： | 飞行仿真 四元数法 气动模型 |
Fighter Flight Simulation System Design |
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| QU Zhi-gang.Fighter Flight Simulation System Design[J].Value Engineering,2012,31(34):184-186. |
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| Authors: | QU Zhi-gang |
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| Institution: | QU Zhi-gang(Naval Aeronautical Engineering Academy Qingdao Campus,Qingdao 266041,China) |
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| Abstract: | In this paper,the design method of the aircraft flight simulation platform was described in detail,taking the F16 aircraft for example,the method can be applied to other aircraft,and can be used for research and simulation on control performance of aircraft flight control system. |
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| Keywords: | flight simulation quaternion method pneumatic model |
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