丁亚林, 仲崇亮, 付金宝. 高马赫飞行条件下光学窗口数学模型的建立[J]. 红外与激光工程, 2013, 42(3): 747-751.
引用本文: 丁亚林, 仲崇亮, 付金宝. 高马赫飞行条件下光学窗口数学模型的建立[J]. 红外与激光工程, 2013, 42(3): 747-751.
Ding Yalin, Zhong Chongliang, Fu Jinbao. Mathematical model of optical window under high-mach flight condition[J]. Infrared and Laser Engineering, 2013, 42(3): 747-751.
Citation: Ding Yalin, Zhong Chongliang, Fu Jinbao. Mathematical model of optical window under high-mach flight condition[J]. Infrared and Laser Engineering, 2013, 42(3): 747-751.

高马赫飞行条件下光学窗口数学模型的建立

Mathematical model of optical window under high-mach flight condition

  • 摘要: 航空遥感器是获取地面信息的重要工具,高马赫飞行条件下光学窗口的数学模型是开展高速航空遥感成像研究的基础。高马赫飞行会对光学窗口的形状和折射率分布造成影响,进而影响遥感器的成像质量。为保证或提高航空遥感器成像质量,需要研究高马赫飞行条件对窗口造成的影响,即建立该条件下光学窗口的数学模型。首先,给出高马赫飞行条件下有关光学窗口的问题描述,并给定输入参数和进行分析的边界条件;然后,分别建立光学窗口的温度场模型和面型模型,并进一步建立折射率与温度间的函数关系;最后,推导得到高马赫飞行条件下光学窗口的数学模型。

     

    Abstract: Aerial remote sensor is very important for obtaining ground information. For high-mach flight condition, the mathematical model of optical window is the foundation for developing research on remote imaging. The shape and refractive index distribution of optical window are affected by high-mach flight condition, so that the image quality of remote sensor would also be affected. It is necessary to establish mathematical model of optical window in order to improve image quality. Firstly, optical window under high-mach flying condition was described and input parameters and boundary conditions of analysis were defined. Secondly, the temperature field model and deformation model of optical window were established. Then, the characteristics of refractive index was presented as a function of temperature. Finally, the mathematical model of optical window under the condition of high-mach flight was derived.

     

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