线性雪崩光电二极管(Avalanche photodiode,APD)焦平面红外探测器有着广泛应用场景,APD探测器耦合具有多种模式的读出电路可在有限像元面积内实现多模式探测,提升探测系统集成度。本文设计了一种具有红外热成像模式、门控3D成像模式、...线性雪崩光电二极管(Avalanche photodiode,APD)焦平面红外探测器有着广泛应用场景,APD探测器耦合具有多种模式的读出电路可在有限像元面积内实现多模式探测,提升探测系统集成度。本文设计了一种具有红外热成像模式、门控3D成像模式、激光测距模式和异步激光脉冲探测模式的APD读出电路,四种模式复用输入级电路。通过Krummenacher结构抑制背景辐射影响,扩展了光子飞行时间探测范围;提出一种改进型时刻鉴别电路,通过减小时刻鉴别误差提升距离测量精度。读出电路采用0.18μm 3.3 V CMOS工艺设计,阵列规模128×128、像元中心距30μm,最大电荷容量3.74 Me^(-)。仿真结果表明,激光测距模式,在积分电容13 f F、背景电流1~150 nA条件下,背景电流响应幅值≤1.35 m V,远小于激光响应电流500 nA时280 m V的响应幅值;异步激光脉冲探测模式的幅值灵敏度约110 nA、脉宽灵敏度约4 ns;改进型时刻鉴别电路对于150~500 nA的激光脉冲响应,时刻鉴别误差约4 ns。本文设计的多模式复用APD读出电路具有一定工程应用价值。展开更多
The nonlinear dynamic model of spinning ballistic missiles is established during the first boosting phase of the missile. Based on the conventional backstepping sliding mode control and the assumption of a two time-sc...The nonlinear dynamic model of spinning ballistic missiles is established during the first boosting phase of the missile. Based on the conventional backstepping sliding mode control and the assumption of a two time-scale separation of missile dynamics, a graded sliding mode controller is designed with two sub-sliding surfaces which have invariability to external disturbances and parameter perturbations, and a matrix which comprises three first order low pass filters is introduced to prevent “explosion of terms”. Owing to the upper bounds of the uncertainties are difficult to obtain in advance, adaptive laws are introduced to estimate the values of the uncertainties in real-time. Eventually, the numerical simulation results given to show the proposed controller can ensure the steady flight of missiles.展开更多
文摘线性雪崩光电二极管(Avalanche photodiode,APD)焦平面红外探测器有着广泛应用场景,APD探测器耦合具有多种模式的读出电路可在有限像元面积内实现多模式探测,提升探测系统集成度。本文设计了一种具有红外热成像模式、门控3D成像模式、激光测距模式和异步激光脉冲探测模式的APD读出电路,四种模式复用输入级电路。通过Krummenacher结构抑制背景辐射影响,扩展了光子飞行时间探测范围;提出一种改进型时刻鉴别电路,通过减小时刻鉴别误差提升距离测量精度。读出电路采用0.18μm 3.3 V CMOS工艺设计,阵列规模128×128、像元中心距30μm,最大电荷容量3.74 Me^(-)。仿真结果表明,激光测距模式,在积分电容13 f F、背景电流1~150 nA条件下,背景电流响应幅值≤1.35 m V,远小于激光响应电流500 nA时280 m V的响应幅值;异步激光脉冲探测模式的幅值灵敏度约110 nA、脉宽灵敏度约4 ns;改进型时刻鉴别电路对于150~500 nA的激光脉冲响应,时刻鉴别误差约4 ns。本文设计的多模式复用APD读出电路具有一定工程应用价值。
文摘The nonlinear dynamic model of spinning ballistic missiles is established during the first boosting phase of the missile. Based on the conventional backstepping sliding mode control and the assumption of a two time-scale separation of missile dynamics, a graded sliding mode controller is designed with two sub-sliding surfaces which have invariability to external disturbances and parameter perturbations, and a matrix which comprises three first order low pass filters is introduced to prevent “explosion of terms”. Owing to the upper bounds of the uncertainties are difficult to obtain in advance, adaptive laws are introduced to estimate the values of the uncertainties in real-time. Eventually, the numerical simulation results given to show the proposed controller can ensure the steady flight of missiles.
