1. 空军工程大学 航空工程学院,西安,710038
2. 解放军95910部队,甘肃,酒泉,735000
3. 空军工程大学 空管领航学院,西安,710051
卢春光(1994—),男,硕士研究生
纸质出版:2019
移动端阅览
卢春光, 周中良, 刘宏强, 等. 量测随机延迟下带非高斯噪声的目标跟踪算法[J]. 哈尔滨工业大学学报, 2019,51(4):83-93.
LU Chunguang, ZHOU Zhongliang, LIU Hongqiang, et al. A target tracking algorithm for zigzag maneuver target tracking with non-gaussian noises and randomly delayed measurements[J]. 2019, 51(4): 83-93.
卢春光, 周中良, 刘宏强, 等. 量测随机延迟下带非高斯噪声的目标跟踪算法[J]. 哈尔滨工业大学学报, 2019,51(4):83-93. DOI: 10.11918/j.issn.0367-6234.201805168.
LU Chunguang, ZHOU Zhongliang, LIU Hongqiang, et al. A target tracking algorithm for zigzag maneuver target tracking with non-gaussian noises and randomly delayed measurements[J]. 2019, 51(4): 83-93. DOI: 10.11918/j.issn.0367-6234.201805168.
为解决量测一步随机延迟及非高斯噪声条件下战斗机蛇形机动模式转弯角速度辨识问题
更好地实现蛇形机动的稳定跟踪
考虑到目标状态与转弯角速度之间相互耦合的特性
基于联合估计与辨识的思想
依据极大似然准则
提出了一种基于期望最大化的目标状态估计与转弯角速度辨识联合优化算法.该算法主体包含两个部分:E-step和M-step.在E-step
首先
通过充分考虑量测一步随机延迟特性及非高斯量测噪声
重新构造了粒子滤波器的似然函数
进而改进了粒子权重的更新公式
同时
为避免粒子贫乏现象的发生
将粒子群优化算法引入到重构的粒子滤波器当中进一步改进粒子采样过程;其次
将拒绝采样思想引入到后向模拟粒子平滑器当中
并相应地设置拒绝采样终止条件
优化后向模拟粒子平滑器
进一步提高平滑算法的执行效率;最后采用改进的粒子滤波器与后向模拟粒子平滑器进一步获取目标状态的平滑量;在M-step
通过采用牛顿迭代法极大化条件似然函数
从而获得转弯角速度的估计量
用于下一次算法迭代.通过E-step和M-step的不断迭代
进而获得转弯角速度的闭环形式的优化解.仿真实验结果表明
所提算法的目标状态估计与角速度辨识的精度均优越于传统的扩维法.
To identify the turn rate of fighter Zigzag maneuver under one-step randomly delayed measurements and non-Gaussian measurements noise and to achieve better tracking performance
based on the idea of joint estimation and identification and Maximum Likelihood Estimation Criteria
a joint optimization algorithm based on expectation maximization for target state estimation and turning angular identification is proposed
which takes mutual coupling between target state and turning angular velocity into account. The algorithm basically contains two parts: E-step and M-step. In the E-step
the likelihood function of particle filter was firstly reconstructed by fully taking one-step randomly delayed measurements and non-Gaussian measurements noise into account
which improves the update formula of particle weight. Meanwhile
in order to avoid particle deficiencies
the particle swarm algorithm was introduced into the reconstructed particle filter to improve the sampling process. Secondly
the idea of rejection sampling was introduced into the backward simulation particle smoother
and the termination condition for rejecting the sampling was set accordingly
thus the backward simulation particle smoother was further optimized to improve the execution efficiency of the smoothing algorithm. Lastly the smooth estimation of the target state was obtained by using the improved particle filter and backward simulation particle smoother. In the M-step
a numerical optimization algorithm was used to maximize the conditional likelihood function
and the estimation of the turning angular velocity was thus obtained for the next iteration of the algorithm. The optimized solution of the closed-loop form of the turning angular velocity was obtained by the iteration of E-step and M-step. Simulation results show that the proposed algorithm performed better in state estimation and turn rate identification than the traditional augmentation method.
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