摘要
微动建模是研究弹道目标微多普勒特征的关键和基础。目前基于Euler角、Euler-Rodrigue公式和齐次坐标的建模方法存在"万向节死锁"、奇异、计算复杂等问题。四元数方法采用4个参数代替矩阵方法的9个参数,能够直观表示三维空间内任意旋转,并克服现有方法的缺陷。经过推导,给出了基于四元数的弹道目标进动和摆动微多普勒数学模型表达式。由于减少了矩阵运算,使得目标微多普勒频率的计算更加简单。仿真结果表明,基于四元数旋转的微动建模方法是合理的,为弹道目标的微多普勒特征提取和识别提供了科学依据。
Micromotion kinetics modeling is a key and fundamental issue of ballistic target microDoppler feature research.At presentthe modeling techniques based on Euler anglesEulerRodrigue formula and homogeneous coordinates have some problems such as “gimbal lock”singularity and computational complexity.Quaternion method can express arbitrary rotation in 3D space intuitively and overcome shortcomings of the existing methods by using 4 values instead of the 9 of the corresponding matrix.The quaternion based precession and wobbling microDoppler frequency expressions of ballistic targets are presented after derivation.It simplifies the calculation of target microDoppler in that reducing matrix operations.The simulation results prove that the quaternion based micromotion modeling method is valid and provides a scientific basis for microDoppler extraction and recognition of ballistic targets.
出处
《电光与控制》
北大核心
2013年第11期65-69,共5页
Electronics Optics & Control
关键词
微多普勒
弹道目标
四元数
目标识别
进动
micro-Doppler
ballistic targets
quaternion
target recognition
precession