| 舵机负载模拟器惯量失配加载补偿方法 |
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| 引用本文： | 陶渝辉,王战.舵机负载模拟器惯量失配加载补偿方法[J].现代防御技术,2012,40(3):178-181. |
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| 作者姓名： | 陶渝辉 王战 |
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| 作者单位： | 北京仿真中心航天系统仿真重点实验室,北京,100854 |
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| 摘 要： | 针对舵机负载力矩模拟器输出等效惯量大于被加载舵机舵面惯量的舵机加载试验情况,研究了其力矩加载补偿方法,分析了其力矩加载误差,提出了针对不同误差源的提高仿真精度的技术途径。分析结果表明,此力矩加载补偿方法现实可行,提高了试验资源的利用率,具有较好的经济效益和现实意义。
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| 关 键 词： | 负载模拟器 惯量 补偿方法 |
Missile Actuator Load Simulator Inertia Mismatch Compensation Methods |
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| TAO Yu-hui
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WANG Zhan.Missile Actuator Load Simulator Inertia Mismatch Compensation Methods[J].Modern Defence Technology,2012,40(3):178-181. |
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| Authors: | TAO Yu-hui WANG Zhan |
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| Institution: | (Beijing Simulation Center,Science and Technology on Space System Simulation Laboratory, Beijing 100854,China) |
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| Abstract: | The compensation methods are discussed when load simulator inertia is greater than missile control surface inertia.Errors of missile actuator torque and deflection angle exist in simulation using compensation.The approaches are presented to improve simulation according to different errors.Analysis results show that the compensation method is useable and valuable to many missile actuator load simulations. |
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| Keywords: | load simulator inertia compensation methods |
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