One size does not fit all: personalized incentives in military compensation

A critical element in implementing a compensation scheme including nonmonetary incentives (NMIs) is recognizing that preferences vary widely across Service members. There are at least three sources of variability: across different population classes, across individuals within a population class, and across NMI packages for a particular individual. Surveys across different military communities, ranks, and years of Service show the difficulty of identifying any NMI that has significant value for even 50% of the active duty force. At the same time, approximately 80% of the surveyed Service members expressed a significant positive value for at least one NMI. Therefore, one-size-fits-all incentive packages will not be nearly as effective as more personalized incentive packages. The authors discuss variability in Service member NMI preferences and outline an approach to implementing personalized NMI packages in military compensation through a sealed-bid reverse auction, where Service members select individual NMIs from a “cafeteria-style” menu of options.     

间距和角度失调对零色散飞秒整形系统的影响

为了研究间距和角度失调对零色散飞秒整形时域特性的影响,理论上分析了系统的分辨率与各光学元件间距角度失调的关系,详细讨论了间距角度失调对系统效率和输出脉冲时间特性的影响.实验结果表明,透镜位置失调会导致脉冲展宽,且两个透镜位置失调对脉宽展宽的规律对称,光栅位置失调也会导致脉冲展宽.此外,器件角度失调对系统效率的影响大于位...     

半带脉冲成形滤波器设计及性能分析

为了减少调制带宽、抑制带外杂散,通信系统中通常在发射端设置脉冲成形滤波器,而为了获得最大信噪比,在接收端通常使用匹配滤波器。以半带滤波器为基础,利用多级级联方法,设计了一种新型的脉冲成形滤波器,通过最小、最大相位分解方法,使得滤波器便于在实际通信系统中的使用。仿真结果表明,设计的成形滤波器与升余弦滚降滤波器相比,通带起伏小,硬件资源耗费少,在低信噪比时对不同调制方式均有额外的功率增益。     

自适应二阶滑模制导律

传统基于Lyapunov定理所设计的制导律无法保证制导系统的有限时间收敛.基于滑模控制理论,给出了一种二阶滑模有限时间收敛方法,并将该方法与机动目标拦截情形相结合,进行制导律的设计.该制导律首项使得视线转率趋于0,而扩展项可满足视线成型,滑模面的有限时间收敛等特性.针对2种典型的目标机动形式进行了仿真研究,结果表明该滑模制导律可以实现目标的有效拦截,满足上述特性.     

基于矩阵乘法的高速卫星成形滤波器的FPGA实现

根据高速8PSK卫星调制器的要求,针对数字化基带成形滤波的信号处理特点,文中提出一种基于矩阵乘法的高速卫星成形滤波器设计方法及基于查找表的硬件实现方案。该方法将成形滤波直接抽象为矩阵乘法的运算,将多个卷积相乘项相加后再量化,减少了量化次数,提高了量化信噪比。用片内的BLOCK-RAM精心设计查找表,在8万门的芯片VIRTEX2-80中就能实现此方案。MODELSIM的时序仿真结果表明,可支持高达200Mbps的输入数据,满足卫星通信高速成形的要求,并针对未来更高速率的成形滤波器给出了一种通用硬件实现方法。     

挠性航天器变幅值输入成形姿态机动策略

针对变参数挠性航天器的姿态机动问题,在变幅值零振动成形器的基础上,提出了鲁棒性较强的变幅值零振动和零微分成形器设计方法,设计了鲁棒姿态机动策略.该机动策略的控制目标是,将航天器机动到期望状态的同时,消除挠性结构的残余振动.以含转动挠性太阳翼的航天器进行三轴姿态机动为例,进行数值仿真.仿真结果表明,该机动策略对挠性结构频...