合成孔径雷达景象匹配中制导导弹定位

研究了合成孔径雷达景象匹配中制导中的导弹定位问题。部分孔径成像是景象匹配中制导合成孔径雷达有效的成像模式,为便于利用多匹配点定位,提出了聚焦多普勒波束锐化成像方法。建立了基于匹配点距离差和多普勒差,并考虑了高度、速度和匹配点位置测量误差的定位模型。推导了位置估计的克拉美-罗下限(Cramer-Rao lower bound,CRLB)。提出了一种基于最小二乘的闭式求解算法。理论分析表明,在一定近似条件下,这一算法的估计精度到达CRLB。仿真分析了各种误差因素对CRLB的影响,验证了算法的理论分析结果及其有效性。

SAR末制导中导弹定位方法及分析

提出导弹在末制导中通过数字景像匹配后 ,采用惯导数据中的一些参数 (如斜距 ,地距 ,速度等 )来确定规则飞行弹体和不规则飞行弹体位置的方法。并分析由于测量数据误差给定位带来的误差大小以及采用 0 .

无源BD在导弹自定位中的应用研究

为了解决近程防空导弹制导雷达实现全方位、高数据率跟踪多目标、截获跟踪多导弹遇到的资源紧张问题,提出了利用BD无源定位方案实现导弹自定位,提高导弹自定位精度的方法。仿真结果表明,该方案合理可行,可降低导弹定位误差,所得结果对防空导弹自定位方案设计具有指导意义。

Three-time rapid transfer alignment method of SINS/GPS navigation system of high-speed marine missile

The transfer alignment of SINS/GPS navigation system of a high-speed marine missile was investigated. With the help of the big acceleration of a high-speed missile, the transfer alignment was changed into a three-time alignment. The azimuth alignment was coarsely finished in 10s in the first time alignment, the horizontal alignment was accurately and rapidly finished in the second time alignment, and the azimuth alignment was accurately finished in the third time alignment. Because the second time alignment and the third time alignment were finished by GPS after the missile was launched, the horizontal alignment and the second azimuth alignment got rid of the influence of the warship body flexibility deforming. The precision and rapidity of the horizontal alignment were prominently increased due to the vertical launch of the marine missile with the big acceleration. Simulation verifies the effectiveness of the proposed alignment method.