设计了一个8×8的Ka频段双圆极化相控阵天线。该天线单元采用正交缝隙耦合馈电的多层贴片微带天线,并由一个小型化宽带3 d B枝节电桥实现双圆极化。为提高天线圆极化性能,依次旋转天线单元,形成2×2双圆极化天线子阵。以天线子...设计了一个8×8的Ka频段双圆极化相控阵天线。该天线单元采用正交缝隙耦合馈电的多层贴片微带天线,并由一个小型化宽带3 d B枝节电桥实现双圆极化。为提高天线圆极化性能,依次旋转天线单元,形成2×2双圆极化天线子阵。以天线子阵为基础,扩展成8×8相控阵天线。HFSS仿真结果表明,天线在方位360°俯仰±60°范围内进行双圆极化扫描,轴比小于3 d B,且轴比带宽达30%。该研究结果可应用于卫星通信的双圆极化相控阵天线的设计。展开更多
An extended Kalman filter with adaptive gain was used to build a miniature attitude and heading reference system based on a stochastie model. The adaptive filter has six states with a time variable transition matrix. ...An extended Kalman filter with adaptive gain was used to build a miniature attitude and heading reference system based on a stochastie model. The adaptive filter has six states with a time variable transition matrix. When the system is in the non-acceleration mode, the accelerometer measurements of the gravity and the compass measurements of the heading have observability and yield good eslimates of the states. When the system is in the high dynamic mode and the bias has converged to an aceurate estimate, the attitude caleulation will be maintained for a long interval of time. The adaptive filter tunes its gain automatically based on the system dynamics sensed by the accelerometers to yield optimal performance,展开更多
文摘设计了一个8×8的Ka频段双圆极化相控阵天线。该天线单元采用正交缝隙耦合馈电的多层贴片微带天线,并由一个小型化宽带3 d B枝节电桥实现双圆极化。为提高天线圆极化性能,依次旋转天线单元,形成2×2双圆极化天线子阵。以天线子阵为基础,扩展成8×8相控阵天线。HFSS仿真结果表明,天线在方位360°俯仰±60°范围内进行双圆极化扫描,轴比小于3 d B,且轴比带宽达30%。该研究结果可应用于卫星通信的双圆极化相控阵天线的设计。
文摘An extended Kalman filter with adaptive gain was used to build a miniature attitude and heading reference system based on a stochastie model. The adaptive filter has six states with a time variable transition matrix. When the system is in the non-acceleration mode, the accelerometer measurements of the gravity and the compass measurements of the heading have observability and yield good eslimates of the states. When the system is in the high dynamic mode and the bias has converged to an aceurate estimate, the attitude caleulation will be maintained for a long interval of time. The adaptive filter tunes its gain automatically based on the system dynamics sensed by the accelerometers to yield optimal performance,
