Description: 这是本战略战术导弹制导的书中的matlab程序,比书中的 forchan程序简单易懂-This is the strategic and tactical missile guidance book of Matlab procedures, the book than a simple understandable forchan Platform: |
Size: 77824 |
Author: |
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Description: 根据导弹仿真数据,绘制可直观显示弹道特性的理想弹道曲线。给出了比例导引法的差分方程,建立了
比例导引法的三维弹道仿真模型。在对比例导引法进行三维弹道仿真的基础上,分别对增量比例导引、基于二次
型的最优制导律和考虑动态特性的二次型最优制导律进行了三维弹道仿真,绘制出了可直观显示弹道特性的理想
弹道,计算了导弹与目标的遭遇时间,并对结果进行了比较分析。最后得出考虑弹体动态特性的二次型最优制导
律具有最优性。-According to the missile simulation data, mapping can be visual display characteristics of an ideal ballistic ballistic curve. Proportional navigation law gives the differential equation, proportional navigation law established a three-dimensional trajectory simulation model. Proportional navigation in the three-dimensional trajectory simulation method, based on the respective proportion of the incremental guidance, based on quadratic optimal guidance law and consider the dynamic characteristics of quadratic optimal guidance law for a three-dimensional trajectory simulation, rendering a visual display may be the ideal ballistic trajectory characteristics, calculated the missile with the target Platform: |
Size: 189440 |
Author:特步 |
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Description: 这本书是导弹制导控制的基本书籍,非常适合初学者使用。-This book is the missile guidance control of the basic books, very suitable for beginners to use. Platform: |
Size: 8843264 |
Author:王宇航 |
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Description: 采用比例导引法,把三维追击轨道分解到两个二维平面上分别导引,并充分考虑到目标的
机动性对弹道的影响,用MATLAB软件编写程序模拟出导弹实际追击的三维变轨弹道,绘制出分运动和合运动中各参数的
变化曲线。最后比较了不同的追击速度和不同的导引系数k对弹道特性的影响,考虑到导弹实际飞行时受需用法向过载的
制约,导出了导引系数k应满足的普遍公式,提出了对实战具有一定参考价值的建议。
-Using proportional navigation law, in pursuit of the three-dimensional orbit decomposition to two two-dimensional plane, respectively, guidance, and taking fully into account the objectives of the impact of mobility on the trajectory, using MATLAB software programming practical pursuit of missile simulated three-dimensional orbit trajectory , to map out points Movement Hop movement curve of each parameter. Finally, the pursuit of different speed and different-guided ballistic coefficient k on the characteristics of, taking into account the actual missile flight by the need to overload the use of constraints derived Seeker coefficient k should satisfy the general formula, put forward on the actual reference value has a certain proposal. Platform: |
Size: 295936 |
Author:李恒 |
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Description: The book presents a historical background of past and present guided missile systems and the evolution of modern weapons,discusses the generalized missile equations of motion, aerodynamic forces and coefficients, the important subject of the various types
of tactical guidance laws and/or techniques, weapon delivery systems and techniques,strategic
missiles and cruise missile theory and
design. Platform: |
Size: 3264512 |
Author:jbarragan |
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Description: 比例导引理想弹道仿真Matlab代码,给出了比例导引法的差分方程, 采用Matlab语言, 对比例导引法的导弹理想弹道进行了三维数据仿真, 绘制出三维理想弹道。随导弹与目标参数变化情况, 对理想弹道的特性进行了分析。-Ideal proportional navigation trajectory simulation Matlab code, the law gives the proportional navigation differential equations using Matlab language, the ideal ratio of ballistic missile guidance method for simulation of three-dimensional data, to map out the ideal three-dimensional trajectory
Platform: |
Size: 1024 |
Author:madier |
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Description: 介绍导弹制导方面的书籍,一本经典的直到方面的外文书籍,希望能对相关专业人士有所帮助-Introduction about missile guidance and control sysytem,you can study missle zhidao system from it
,Most air defense systems in use or under development today, employ homing
guidance to effect intercept of the target. By virtue of the use of onboard data
gathering, the homing guidance system provides continually improving quality of
target information right up to the intercept point. More than any single device, the
guided missile has shaped the aerospace forces of the world today. Combat aircraft,
for example, are fitted with airborne weapons that can be launched against enemy
aircraft, ground forces, or strategic targets deep inside enemy territory. Also, the
guided missile can be employed as a diversionary weapon to confuse ground and
air forces. Ground-based missile systems have various range capabilities from a few
miles to several thousand miles. These ground-based missiles are ballistic or nonballistic
types, depending on their mission requirements. The design of a gu Platform: |
Size: 3037184 |
Author:liuhazi |
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Description: 运用导弹比例导引法原则,在matlab中实现三维视图仿真。-The proportion of the use of the missile guidance law principles, to achieve three-dimensional view in the matlab simulation. Platform: |
Size: 1024 |
Author:fang |
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Description: 先进空空导弹最优中制导律研究Advanced Missile Guidance Law of the best in the-Advanced Missile Guidance Law of the best in the Platform: |
Size: 454656 |
Author:atoz123 |
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Description: 导弹内部控制系统的设计。包括导弹制导,导弹飞行,导弹控制,通信传输等等部分。-Missile internal control system design. Including missile guidance, missile flight, missile control, communications, transport and so on parts. Platform: |
Size: 6786048 |
Author:刘睿智 |
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Description: 导弹制导律辨识,算法基于IMM,仿真效果比较好,可以使用。(Missile guidance law identification, based on IMM.Simulation effect is OK, you can use.) Platform: |
Size: 5120 |
Author:快捷键2 |
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