检索规则说明:AND代表“并且”;OR代表“或者”;NOT代表“不包含”;(注意必须大写,运算符两边需空一格)
检 索 范 例 :范例一: (K=图书馆学 OR K=情报学) AND A=范并思 范例二:J=计算机应用与软件 AND (U=C++ OR U=Basic) NOT M=Visual
作 者:梁津鑫 唐奇 崔颢[1,3] 张公平 Liang Jinxin;Tang Qi;Cui Hao;Zhang Gongping(China Airborne Missile Academy,Luoyang 471009,China;Unit 93160 of PLA,Beijing 100076,China;National Key Laboratory of Air-based Information Perception and Fusion,Luoyang 471009,China)
机构地区:[1]中国空空导弹研究院,河南洛阳471009 [2]中国人民解放军93160部队,北京100076 [3]空基信息感知与融合全国重点实验室,河南洛阳471009
出 处:《航空兵器》2024年第5期82-87,共6页Aero Weaponry
基 金:航空科学基金项目(201901012008)。
摘 要:针对传统滤波算法在处理目标复杂机动时非线性逼近能力不足、跟踪精度下降等问题,提出一种强跟踪容积卡尔曼滤波(STCKF)方法。首先,根据战斗机规避空空导弹的机动特征,建立了蛇形机动和桶滚机动两种目标运动模型;其次,引入强跟踪滤波(STF)以增强容积卡尔曼滤波(CKF)对系统状态突变等不确定因素的能力;然后,将STCKF应用于导弹末制导目标运动参数估计中,并通过与CKF、无迹卡尔曼滤波(UKF)和粒子滤波(PF)的对比仿真分析验证了该方法的有效性。仿真结果表明,STCKF具有较强的鲁棒性和系统自适应能力,尤其在目标机动突变时其跟踪误差相比CKF减小约10%,能够满足空空导弹末制导高精度和快速响应要求。A strong tracking cubature Kalman filter(STCKF)method is proposed to overcome the challenges of insufficient nonlinear approximation capability and decreased tracking accuracy of traditional filtering algorithms in dealing with complex maneuvering targets.Firstly,models for snake maneuver and barrel roll maneuver are developed based on the maneuvering characteristics of fighter aircraft evading air-to-air missiles.Secondly,strong tracking filter(STF)is introduced to enhance the ability of cubature Kalman filter(CKF)to handle sudden changes in system states and other uncertainties.Then,STCKF is applied to estimate the motion parameters of missile terminal guidance target,and its effectiveness is validated through comparative simulation analysis with CKF,unscented Kalman filter(UKF),and particle filter(PF).Simulation results indicate that STCKF has enhanced robustness and adaptive capabilities,especially when the target maneuver suddenly changes,its tracking error is reduced by about 10%compared to CKF,which can meet the high precision and rapid response requirements of air-to-air missile terminal guidance.
关 键 词:容积卡尔曼滤波 强跟踪滤波 非线性滤波 目标跟踪 空空导弹 制导
分 类 号:TJ765[兵器科学与技术—武器系统与运用工程] V249[航空宇航科学与技术—飞行器设计]
正在载入数据...
正在载入数据...
正在载入数据...
正在载入数据...
正在载入数据...
正在载入数据...
正在载入数据...
正在链接到云南高校图书馆文献保障联盟下载...
云南高校图书馆联盟文献共享服务平台 版权所有©
您的IP:216.73.216.7