| 高超速飞行器纵向模型建模研究 |
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| 引用本文： | 张红梅.高超速飞行器纵向模型建模研究[J].沈阳航空工业学院学报,2010,27(2):8-10. |
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| 作者姓名： | 张红梅 |
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| 作者单位： | 沈阳航空工业学院,辽宁,沈阳,110136 |
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| 摘 要： | 针对高超音速飞机纵向模型的高度非线性、强耦合、参数不确定等特点,提出了基于sim-link的建模方法。并基于所建模块用trim函数得到飞行状态的平衡点。所得结果可用于高超音速飞行器的控制器设计和仿真研究。
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| 关 键 词： | 高超音速飞机 建模 平衡状态 |
Modeling and simulation research on a hypersonic vehicle |
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| ZHANG Hong-mei.Modeling and simulation research on a hypersonic vehicle[J].Journal of Shenyang Institute of Aeronautical Engineering,2010,27(2):8-10. |
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| Authors: | ZHANG Hong-mei |
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| Institution: | ZHANG Hong-mei (Shenyang Institute of Aeronautical Engineering,Liaoning Shenyang 110136) |
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| Abstract: | A generic nonlinear longitudinal dynamics model for hypersonic vehicle is given in Matlab/simlink,which includes strong nonlinear,coupling and parameters uncertainty.With function trim in matlab,the equilibrium state is got based on proposed model.Results can be used to control design and simulation research efficient. |
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| Keywords: | hypersonic vehicle modeling equilibrium state |
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