| 无人机飞行控制仿真系统研究 |
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| 引用本文： | 周志久,韦闽峰.无人机飞行控制仿真系统研究[J].航天控制,2010,28(1). |
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| 作者姓名： | 周志久 韦闽峰 |
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| 作者单位： | 北京航天自动控制研究所,北京,100854 |
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| 摘 要： | 针对某型无人机的研制开发,提出了可行的仿真系统设计方案。首先设计全数字仿真验证飞行控制律的有效性,在此基础上,根据使用条件的差异,设计了两种相互关联的半物理仿真系统,即不带转台的半物理仿真以及带转台的半物理仿真,用来模拟无人机的飞行状况。最后给出了仿真的部分曲线。仿真结果表明,以上这种仿真系统可以对整个无人机飞控系统设计的合理性及有效性进行完备的验证,对同类飞行器仿真系统的研发具有一定的参考价值。
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| 关 键 词： | 无人机 飞行控制 数字仿真 半物理仿真 |
Research on Flight Control Simulation System of UAV |
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| ZHOU Zhijiu,WEI Minfeng.Research on Flight Control Simulation System of UAV[J].Aerospace Control,2010,28(1). |
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| Authors: | ZHOU Zhijiu WEI Minfeng |
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| Institution: | ZHOU Zhijiu WEI MinfengBeijing Aerospace Automatic Control Institute,Beijing 100854,China |
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| Abstract: | The scheme of developing a UAV simulation system is proposed regarding the research of concern type.Firstly,the validity of fight control laws is verified by the simulation test with full digital mode.Based on the validity course,two correlative semi-physical simulation systems are both designed according to different conditions to simulate flight status of UAV,which are separated with turntable function and without turntable function.Finally,partial curves of simulation are illustrated.The simulation resul... |
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| Keywords: | UAV Flight control Digital simulation Semi-physical simulation |
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