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[OtherMissileGuidanceSimuDemo01

Description: 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
Platform: | Size: 8192 | Author: donotspam | Hits:

[matlabzyzd

Description: 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.
Platform: | Size: 2048 | Author: stephen | Hits:

[OtherCOM_imm

Description: 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
Platform: | Size: 2048 | Author: zhangsheng | Hits:

[OtherCS

Description: 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
Platform: | Size: 2048 | Author: zhangsheng | Hits:

[OtherEKF

Description: 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
Platform: | Size: 1024 | Author: zhangsheng | Hits:

[Windows DevelopDraw

Description: 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
Platform: | Size: 1024 | Author: zhangsheng | Hits:

[Software EngineeringGA_missile_trajectory_simulation

Description: 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.
Platform: | Size: 25600 | Author: 木木 | Hits:

[SCMUntitled2

Description: 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
Platform: | Size: 1024 | Author: winwind | Hits:

[matlabProportionalnavigationmethod

Description: 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.
Platform: | Size: 1024 | Author: 康凯 | Hits:

[Software Engineeringabout-target-tracker

Description: 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
Platform: | Size: 267264 | Author: 黄渤蛟 | Hits:

[Software Engineering3

Description: 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
Platform: | Size: 192512 | Author: jiajie | Hits:

[matlabKalmanfilter

Description: 弹道导弹跟踪过程中的Kalman滤波应用-Application of Kalman filter in ballistic missile tracking
Platform: | Size: 406528 | Author: 王小超 | Hits:

[matlabEx15_2_ParticleEx2

Description: 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.
Platform: | Size: 2048 | Author: 戴洪德 | Hits:

[matlabballistic

Description: 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
Platform: | Size: 1024 | Author: 王文博 | Hits:

[Industry researchTarget-Tracking

Description: 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.
Platform: | Size: 1046528 | Author: 秋槐 | Hits:

[matlabIMM_PF

Description: IMM Particle Filter for ballistic projectile tracking
Platform: | Size: 8192 | Author: Ozan Bilgin | Hits:

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