中国公司治理的路径依赖——理论与实证分析

1Introduction　Now ,in orbitspacecraftsdeveloprapidlyinqualityandquantity,whilethegroundTT&Cresourceisrelativelylimi ted .Therefore ,torealizespacecraftautonomousnavigationandpositioningseemsespeciallytobeimportant.Itisoneoftheimportantaspectstoincreasethein orbitspacecraftself containedability .　ExtensiveattentionshavebeenpaidtotheapplicationofGPSinthisarea,andquiteanumberofachievementshavebeengained ,butitisonlythebeginning .　FortheutilizationofGPSinspacecraftnavigationandpo sitioning …     

高速公路平曲线标志标线组合设计评价指标

基于驾驶模拟实验数据,结合驾驶员在高速公路平曲线的运行速度特征、转向特征与行驶轨迹特征,选择速度、方向盘转角系数与横向位置数据构建了高速公路平曲线标志标线组合设计的合理性评价指标与有效性评价指标.其中,合理性评价指标包括转向位置的合理性评价与驾驶负荷的合理性评价,采用小波分解的方法对方向盘转角系数进行多层分解,获取驾驶员转向起终点位置与高频能量,通过驾驶员转向起终点与直缓点/缓直点的距离进行转向位置的合理性评价,通过高频能量比进行驾驶员操作负荷的合理性评价.有效性评价包括运行速度控制的有效性与车辆横向位置控制的有效性,通过平均速度、运行速度与车速离散度进行速度控制效果的评价;通过平均换道次数、平均压线行驶距离进行车辆横向位置控制的有效性评价.通过实例应用验证了研究标志标线组合设置的必要性与评价指标的有效性.     

旋转弹引信用卫星定位接收信号旋转解调方法

为解决旋转弹飞行中的高旋转、高动态条件会造成卫星定位接收系统无法正常定位的问题,针对旋转、动态环境开展了旋转弹卫星定位接收信号旋转解调方法的研究.详细分析了旋转条件对卫星定位信号接收的影响,并针对旋转特性设计了旋转跟踪解调环,用于对旋转的跟踪与解调,给出了旋转弹卫星定位信号接收系统的设计方案,基于Simulink实现了旋转弹卫星定位信号接收系统的仿真,并给出了相应的仿真与实验结果.结果表明,设计的以旋转跟踪环为核心的旋转弹卫星定位信号接收系统,在中心频率为200 Hz的情况下跟踪范围可达到±40 Hz,较好地满足了转速在200转/s左右的旋转弹信号接收要求.      

《三国演义》中的梦境管窥

《三国演义》中的梦分喜梦和凶梦两种，喜梦为帝王预兆和象征，凶梦预兆国家易主或小说中重要人物的死亡，两种梦对人物形象的塑造和故事情节的推动，均有不可忽视的重要作用。     

New rapid transfer alignment method for SINS of airborne weapon systems

Transfer alignment is an effective alignment method for the strapdown inertial navigation system （SINS） of airborne weapon systems. The traditional transfer alignment methods for large misalignment angles alignment use nonlinear transfer align- ment models and incorporate nonlinear filtering. A rapid transfer alignment method with linear models and linear filtering for ar- bitrary misalignment angles is presented. Through the attitude quaternion decomposition, the purpose of transfer alignment is converted to estimate a constant quaternion. Employing special manipulations on measurement equation, velocity and attitude linear measurement equations are derived. Then the linear trans- fer alignment model for arbitrary misalignment angles is built. An adaptive Kalman filter is developed to handle modeling errors of the measurement noise statistics. Simulation results show feasibili- ty and effectiveness of the proposed method, which provides an alternative rapid transfer alignment method for airborne weapons.     

Self-alignment of full skewed RSINS：observability analysis and full-observable Kalman filter

Traditional orthogonal strapdown inertial navigation sys-tem （SINS） cannot achieve satisfactory self-alignment accuracy in the stationary base： taking more than 5 minutes and al the iner-tial sensors biases cannot get ful observability except the up-axis accelerometer. However, the ful skewed redundant SINS （RSINS） can not only enhance the reliability of the system, but also improve the accuracy of the system, such as the initial alignment. Firstly, the observability of the system state includes attitude errors and al the inertial sensors biases are analyzed with the global perspective method： any three gyroscopes and three accelerometers can be assembled into an independent subordinate SINS （sub-SINS）;the system state can be uniquely confirmed by the coupling connec-tions of al the sub-SINSs;the attitude errors and random constant biases of al the inertial sensors are observable. However, the ran-dom noises of the inertial sensors are not taken into account in the above analyzing process. Secondly, the ful-observable Kalman filter which can be applied to the actual RSINS containing random noises is established; the system state includes the position, ve-locity, attitude errors of al the sub-SINSs and the random constant biases of the redundant inertial sensors. At last, the initial self-alignment process of a typical four-redundancy ful skewed RSINS is simulated： the horizontal attitudes （pitch, rol ） errors and yaw error can be exactly evaluated within 80 s and 100 s respectively, while the random constant biases of gyroscopes and accelero-meters can be precisely evaluated within 120 s. For the ful skewed RSINS, the self-alignment accuracy is greatly improved, mean-while the self-alignment time is widely shortened.     

一种有效估计着陆引导信号多径时延的方法

利用导航信号收发已知且具有周期性的特点,提出了一种对着陆引导信号多径时延进行有效估计的方法。该方法首先计算相关函数,而后对相关函数进行二次微分,对时延值进行初步估计。最后通过直线拟合算法和比例拟合算法提高估计精度。通过计算机仿真,验证了算法的有效性。该算法具有在低采样率的条件下,估计精度高的特点。     

GPSNISNAV integrated relative navigation and attitude determination system for ultra-close spacecraft formation flying

For the improvement of accuracy and better fault-tolerant performance, a global position system (GPS)/vision navigation (VISNAV) integrated relative navigation and attitude determination approach is presented for ultra-close spacecraft formation flying. Onboard GPS and VISNAV system are adopted and a federal Kalman filter architecture is used for the total navigation system design. Simulation results indicate that the integrated system can provide a total improvement of relative navigation and attitude estimation performance in accuracy and fault-tolerance.     

千枚岩隧道破碎带 TSP 超前预报解译标志

千枚岩等软岩隧道施工中易出现垮塌等地质灾害。以典型千枚岩隧道———汶马高速公路鹧鸪山隧道为例,以地震波传播理论为依据,结合工程地质分析及地震波正演模拟,探讨TSP 预报中针对千枚岩构造破碎带在不同含水率状况下的地震波反射特性及解译标志,结果表明：纵波及横波遇千枚岩构造破碎带反射现象明显,横波较纵波反射更强烈;破碎带富水时,千枚岩泥化变软,纵波反射加强;从深度偏移角度分析,破碎带内正负反射频繁变化,单个反射层延伸性差。研究结果可以提高 TSP 在软岩隧道中的预报准确性。     

两时间尺度的捷联速度算法研究

根据奇异摄动理论分析具有小参数的捷联惯导系统方程,在两时间尺度上对系统状态方程进行了降阶简化处理,设计捷联算法.在内回路推力速度矢量计算中,应用一种新的划船补偿算法补偿比力转换过程中载体姿态变化产生的速度误差.在外回路中进行重力地速计算,完成导航坐标系上速度的更新.仿真结果表明:新算法精度与Savage四子样算法近似,计算量小.