Search - ballistic tracking

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[Other] MissileGuidanceSimuDemo01 DL : 0: 本程序包为导弹追踪导引法的相对弹道簇图MATLAB仿真计算程序。关键词：导弹弹道追踪导引仿真 missile simulation guidance MATLAB -The package for the missile guidance law to track the relative ballistic cluster map MATLAB simulation program. Key words: ballistic missile tracking guided missile simulation guidance MATLAB simulation
Update : 2025-03-07 Size : 8kb Publisher : donotspam
[matlab] zyzd DL : 0: 最优制导律反战术弹道导弹TBM弹道仿真，matlab编写。-Optimal Guidance Law TBM anti-tactical ballistic missile trajectory simulation, matlab prepared.
Update : 2025-03-07 Size : 2kb Publisher : stephen
[Other] COM_imm DL : 1: This paper studies the problem of tracking a ballistic object in the reentry phase by processing radar measurements. A suitable (highly nonlinear) model of target motion is developed and the theoretical Cramer—Rao lower bounds (CRLB) of estimation error are derived. The estimation performance (error mean and-This paper studies the problem of tracking a ballistic object inthe reentry phase by processing radar measurements. A suitable (highly nonlinear) model of target motion is developed and thetheoretical Cramer-Rao lower bounds (CRLB) of estimationerror are derived. The estimation performance (error mean and
Update : 2025-03-07 Size : 2kb Publisher : zhangsheng
[Other] CS DL : 2: This paper studies the problem of tracking a ballistic object in the reentry phase by processing radar measurements. A suitable (highly nonlinear) model of target motion is developed and the theoretical Cramer—Rao lower bounds (CRLB) of estimation error are derived. The estimation performance (error mean and-This paper studies the problem of tracking a ballistic object inthe reentry phase by processing radar measurements. A suitable (highly nonlinear) model of target motion is developed and thetheoretical Cramer-Rao lower bounds (CRLB) of estimationerror are derived. The estimation performance (error mean and
Update : 2025-03-07 Size : 2kb Publisher : zhangsheng
[Other] EKF DL : 0: This paper studies the problem of tracking a ballistic object in the reentry phase by processing radar measurements. A suitable (highly nonlinear) model of target motion is developed and the theoretical Cramer—Rao lower bounds (CRLB) of estimation error are derived. The estimation performance (error mean and-This paper studies the problem of tracking a ballistic object inthe reentry phase by processing radar measurements. A suitable (highly nonlinear) model of target motion is developed and thetheoretical Cramer-Rao lower bounds (CRLB) of estimationerror are derived. The estimation performance (error mean and
Update : 2025-03-07 Size : 1kb Publisher : zhangsheng
[Windows Develop] Draw DL : 0: This paper studies the problem of tracking a ballistic object in the reentry phase by processing radar measurements. A suitable (highly nonlinear) model of target motion is developed and the theoretical Cramer—Rao lower bounds (CRLB) of estimation error are derived. The estimation performance (error mean and-This paper studies the problem of tracking a ballistic object inthe reentry phase by processing radar measurements. A suitable (highly nonlinear) model of target motion is developed and thetheoretical Cramer-Rao lower bounds (CRLB) of estimationerror are derived. The estimation performance (error mean and
Update : 2025-03-07 Size : 1kb Publisher : zhangsheng
[Software Engineering] GA_missile_trajectory_simulation DL : 1: 提出了一种空面导弹下滑段、俯冲攻击段的弹道优化设计方案,以及一种实现航向动态跟踪的具体方法。大量算例表明,采用本文中的空面导弹控制方案可以设计、调试出较满意的弹道,达到获取导弹飞行性能数据并验证导弹总体设计参数的目的。 -A decline in air-surface missile paragraph, paragraph ballistic dive attack to optimize the design of programs, as well as a course to achieve dynamic tracking of specific methods. A large number of examples show that the use of space in this article surface missile control program can design, debug a more satisfactory trajectory to obtain the missile flight performance data and verify the purpose of missile design parameters.
Update : 2025-03-07 Size : 25kb Publisher : 木木
[SCM] Untitled2 DL : 0: 一种基于弹道模型的机动目标跟踪算法 !针对当前目标跟踪算法中跟踪模型与现代反舰导弹实际运动不匹配而影响跟踪精度的问题!根据反舰导弹的弹道特点!通过分析导弹受力情况和运动状态的关系!提出了一种基于弹道模型的机动目标跟踪算法!并针对高速跃升俯冲运动!分别与基于L:$L=模型的目标跟踪算法作了性能比较仿真结果表明!该算法在原理上是正确可行的!可显著提高对高速强机动目标的跟踪性能-a maneuvering target tracking algorithm based on ballistic model
Update : 2025-03-07 Size : 1kb Publisher : winwind
[matlab] Proportionalnavigationmethod DL : 0: 用比例导引法进行拦截弹针对机动目标的弹道仿真，仿真是基于三维模型。-Proportional navigation method used to intercept ballistic missile targets for motor simulation, simulation is based on three-dimensional model.
Update : 2025-03-07 Size : 1kb Publisher : 康凯
[Software Engineering] about-target-tracker DL : 0: 第二代宙斯盾弹道导弹防御系统成功完成目标追踪演习-The second generation of Aegis ballistic missile defense system successfully target tracking exercise
Update : 2025-03-07 Size : 261kb Publisher : 黄渤蛟
[Software Engineering] 3 DL : 0: 弹道导弹对拦截弹仅测角被动跟踪的可观测性分析，弹道导弹对拦截弹仅测角被动跟踪的可观测性分析-Ballistic missile interceptor missile angle measurement only passive tracking observability analysis, ballistic missile interceptor missile angle measurement only passive tracking observability analysis
Update : 2025-03-07 Size : 188kb Publisher : jiajie
[matlab] Kalmanfilter DL : 0: 弹道导弹跟踪过程中的Kalman滤波应用-Application of Kalman filter in ballistic missile tracking
Update : 2025-03-07 Size : 397kb Publisher : 王小超
[matlab] Ex15_2_ParticleEx2 DL : 2: 粒子滤波目标跟踪程序，地面雷达跟踪一个下落物体的弹道系数、速度和位置。-Particle filter target tracking procedures, ground radar tracking ballistic coefficient, velocity and position of a falling object.
Update : 2025-03-07 Size : 2kb Publisher : 戴洪德
[matlab] ballistic DL : 1: 基于MATLAB的追踪法弹道仿真源代码，简洁有效、运行时间短-Tracking trajectory simulation method
Update : 2025-03-07 Size : 1kb Publisher : 王文博
[Industry research] Target-Tracking DL : 0: 关于弹道目标实时跟踪，有详细的模型和算法策略.-Real-time tracking of ballistic target, have a detailed strategy model and algorithm.
Update : 2025-03-07 Size : 1022kb Publisher : 秋槐
[matlab] IMM_PF DL : 0: IMM Particle Filter for ballistic projectile tracking
Update : 2025-03-07 Size : 8kb Publisher : Ozan Bilgin