微光像增强器是微光成像系统的核心部分,其成像质量决定了对微弱光学信号的探测能力。像增强器的调制传递函数(modulation transfer function,MTF)反映了系统对图像不同频率成分的传递能力,是像质评定的一种客观指标。本文基于狭缝法测...微光像增强器是微光成像系统的核心部分,其成像质量决定了对微弱光学信号的探测能力。像增强器的调制传递函数(modulation transfer function,MTF)反映了系统对图像不同频率成分的传递能力,是像质评定的一种客观指标。本文基于狭缝法测试MTF的原理,进行系统校准和采用分段加权最小二乘拟合实现曲线的平滑去噪,构建了微光像增强器的MTF测试系统。具体是采用十字狭缝靶标进行测试得到线扩散函数(line spread function,LSF)曲线,然后对其进行去噪处理和离散傅里叶变换得到MTF曲线,测试结果与德国OEG-2MTF测试仪比较,误差率低于5%,为研制高成像质量微光像增强器提供了一种有效评价手段。展开更多
In order to better study the dynamic characteristics and the control strategy of parafoil systems,considering the effect of flap deflection as the control mechanism and regarding the parafoil and the payload as a rigi...In order to better study the dynamic characteristics and the control strategy of parafoil systems,considering the effect of flap deflection as the control mechanism and regarding the parafoil and the payload as a rigid body,a six degrees-of-freedom(DOF)dynamic model of a parafoil system including three DOF for translational motion and three DOF for rotational motion,is established according to the K rchhoff motion equation.Since the flexible winged paafoil system flying at low altitude is more susceptibleto winds,the motion characteristics of the parafoil system Wth and Wthout winds are simulated and analyzed.Furthermore,the ardropm test is used to further verify the model.The comparison results show that the simulation trajectory roughly overlaps with the actual flight track.The horzontnl velocity of the simulation model is in good accordance with the airdrop test,with a deviation less than0.5m/s,while its simulated vertical velocity fuctuates slightly under the infuence of the wind,and shows a similar trend to the ardrop test.It is concludedthat the established model can well describe the characteristics of the parafoil system.展开更多
文摘微光像增强器是微光成像系统的核心部分,其成像质量决定了对微弱光学信号的探测能力。像增强器的调制传递函数(modulation transfer function,MTF)反映了系统对图像不同频率成分的传递能力,是像质评定的一种客观指标。本文基于狭缝法测试MTF的原理,进行系统校准和采用分段加权最小二乘拟合实现曲线的平滑去噪,构建了微光像增强器的MTF测试系统。具体是采用十字狭缝靶标进行测试得到线扩散函数(line spread function,LSF)曲线,然后对其进行去噪处理和离散傅里叶变换得到MTF曲线,测试结果与德国OEG-2MTF测试仪比较,误差率低于5%,为研制高成像质量微光像增强器提供了一种有效评价手段。
基金The National Natural Science Foundation of China(No.61273138,61573197)the National Key Technology R&D Program(No.2015BAK06B04)+1 种基金the Key Fund of Tianjin(No.14JCZDJC39300)the Key Technologies R&D Program of Tianjin(No.14ZCZDSF00022)
文摘In order to better study the dynamic characteristics and the control strategy of parafoil systems,considering the effect of flap deflection as the control mechanism and regarding the parafoil and the payload as a rigid body,a six degrees-of-freedom(DOF)dynamic model of a parafoil system including three DOF for translational motion and three DOF for rotational motion,is established according to the K rchhoff motion equation.Since the flexible winged paafoil system flying at low altitude is more susceptibleto winds,the motion characteristics of the parafoil system Wth and Wthout winds are simulated and analyzed.Furthermore,the ardropm test is used to further verify the model.The comparison results show that the simulation trajectory roughly overlaps with the actual flight track.The horzontnl velocity of the simulation model is in good accordance with the airdrop test,with a deviation less than0.5m/s,while its simulated vertical velocity fuctuates slightly under the infuence of the wind,and shows a similar trend to the ardrop test.It is concludedthat the established model can well describe the characteristics of the parafoil system.
