首页> 外文会议>Japan-USA Symposium on Flexible Automation >THE DEVELOPMENT OF AN INERTIAL REFERENCE UNIT (IRU) APPLICABLE TO LASER WEAPON POINTING SYSTEMS
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THE DEVELOPMENT OF AN INERTIAL REFERENCE UNIT (IRU) APPLICABLE TO LASER WEAPON POINTING SYSTEMS

机译:适用于激光武器指向系统的惯性参考单元(IRU)的开发

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Airborne laser systems are directed energy weapons designed to defend against enemy missile attacks. These systems must be able to accurately and steadily track a target from several hundred miles away. Errors in the pointing of the laser beam at the target reduce the accuracy and lethality of the weapon system. There are two types of pointing errors: bias errors and jitter errors. Bias errors are pointing errors that do not change over time and cause the beam to partially or completely miss the target. Jitter errors are oscillations of the beam around the target that spread the beam over a larger area, thereby reducing the energy density of the beam impinging on the target and decreasing the probability of a kill. Jitter errors are usually the result of vibrations of the optical platform and vibrations between the different optical components mounted to the platform. The purpose of the IRU is to reduce the jitter errors of the system by providing an inertially stable reference beam that can be used as part of a feedback control system to measure and eliminate the jitter in the laser pointing system. The IRU works in conjunction with a fast-steering mirror and a detector to measure and correct jitter errors occurring within the optics of the laser pointing system. A single-axis IRU prototype with an outer-axis large angle positioner was designed and modeled. The outer-axis assembly is driven by a DC motor and its purpose is to extend the IRU's range and also provide a source for input disturbances that the IRU will attempt to cancel. An analog feedback control system was developed to close loops around the IRU and outer-axis assembly that will provide two modes of control; large angle positioning and IRU rate-stabilized mode. After the prototype has been fabricated and assembled, the IRU will be tested by driving the outer-axis assembly in an oscillatory fashion to create a base disturbance that the IRU will attempt to cancel. The finished mechanism will be primarily used as a laboratory instructional tool to demonstrate the principles of classical control theory.
机译:空中激光系统是针对旨在防御敌方导弹攻击的能量武器。这些系统必须能够准确,稳定地跟踪几百英里远的目标。目标的指向目标的误差降低了武器系统的准确性和致命性。有两种类型的指向错误:偏置错误和抖动错误。偏差错误指向不随时间变化的错误并导致光束部分或完全错过目标。抖动误差是围绕着较大区域的射梁周围的光束的振荡,从而降低了撞击目标的光束的能量密度并降低杀死的概率。抖动误差通常是光学平台的振动的结果,以及安装在平台上的不同光学元件之间的振动。 IRU的目的是通过提供惯性稳定的参考光束来减少系统的抖动误差,该光束可以用作反馈控制系统的一部分来测量和消除激光指示系统中的抖动。 IRU与快速转向镜和检测器一起工作,以测量和纠正在激光指示系统的光学内发生的抖动误差。设计并建模了具有外轴大角度定位器的单轴IRU原型。外轴组件由直流电动机驱动,其目的是扩展IRU的范围,并提供IRU将尝试取消的输入干扰的源。模拟反馈控制系统是开发的,以围绕IRU和外轴组件封闭环绕,将提供两种控制模式;大角度定位和IRU速率稳定模式。在制造和组装原型之后,IRU将通过驱动外轴组件以振荡方式驱动,以产生IRU将尝试取消的基础干扰。成品机制主要用作实验室教学工具,以证明古典控制理论的原则。

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