| 地空导弹气压舵机仿真数学模型及其校准 |
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| 引用本文： | 王盛山.地空导弹气压舵机仿真数学模型及其校准[J].航天控制,1991(1). |
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| 作者姓名： | 王盛山 |
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| 作者单位： | 航空航天部三○二所 |
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| 摘 要： | 本文给出了某种地一空导弹气压舵机的仿真数学模型,此模型计入了一些重要的非线性因素;介绍了空载校准,仿真试验和导弹飞行验证的综合校准此模型的方法。飞行试验表明此模型具有较高的置信度。
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| 关 键 词： | ~+气压舵机 数学模型 仿真技术 控制系统 地—空导弹 |
A SIMULATED MATHEMATICS MODEL OF GROUND TO AIR MISSILE'S PNEUMATIC ACTUATOR AND ITS CHECKING METHOD |
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| Wang Shengshan.A SIMULATED MATHEMATICS MODEL OF GROUND TO AIR MISSILE''''S PNEUMATIC ACTUATOR AND ITS CHECKING METHOD[J].Aerospace Control,1991(1). |
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| Authors: | Wang Shengshan |
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| Institution: | Wang Shengshan |
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| Abstract: | The paper provides a simulated mathematics model of the ground to air missile's pneumatic actuator in that some major nonlinear factors were considered, presents three methods, no-load check, simulation test and flight test, to check this model. Flight test shows that the confidence of this model is higher. |
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| Keywords: | ~+Pneumatic actuator Mathematical model Simulation technique Control system Ground to air missile |
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