Trajectory planning of the television - guided and air - to - ground missile 水下弹丸速度拟合方法的误差分析
Analysis of air - to - ground missile countermine simulation system based on uml 的空地导弹攻防对抗仿真系统研究
Research on the damage potential of tv - command - guided air - to - ground missiles 电视指令制导空地导弹对目标的毁伤性能研究
Research on the vertical intercept terminal guidance system of tv - command - guidance air - to - ground missile 电视指令制导空地导弹垂直命中目标的末制导系统研究
Air - to - ground missile ( agm ) provides intuitionistic observation plat for agm tactical application and coordinated operation 开发的空对地导弹三维动画系统为空对地导弹的战术应用、协调作战提供了直观的观察平台。
Using the theory of virtual reality we develop the system of engine testing and the system of air - to - ground missile ( agm ) in vc + + 在vc + +环境中,利用虚拟现实的原理设计开发了发动机试车三维动画系统和空对地导弹三维动画系统。
Finally , we develop 3d animation simulation software , which vividly demonstrates the process when air - to - ground missile is attacking certain ground target 最后,本文编制了三维动画可视化仿真软件,生动形象地演示了空地导弹攻击目标的过程。
Anti - radiation missile ( arm ) is an air - to - air or air - to - ground missile that can seek , track and destroy radar systems by making use of electromagnetic wave of the radar beaming , which is also called anti - radar missile 反辐射导弹( anti - radiation - missile , arm )是一种利用雷达辐射源发射的电磁波,发现、跟踪并摧毁雷达系统的空空、空地机载导弹,也称为反雷达导弹。
Then we analyzed the change process of trajectory in air - to - ground missile attack , built the movement equations based on the center of gravity of every segment . in the end we gave the whole trajectory simulation result of air - to - ground attack 分析了空地导弹攻击的弹道变化过程,将攻击过程划分为五部分,分别对各段建立了重心运动方程并进行了仿真,最后给出了空地导弹攻击的全过程弹道仿真结果。
Based on optimal control theory and singularly perturbed theory , a singularly perturbed midcourse guidance law that guarantees air - to - ground missiles to ascent quickly is proposed . this new guidance law is a composite control law consisting of three parts : optimal climbing control using variable weighting factor method , minimum energy cruising phase control and minimum energy switching phase control . moreover , a new control logic is designed in order to remove influence of climbing control on switching phase . simulation results of a certain type of air - to - ground missile are presents . it is shown that , with simple control algorithm and feasible onboard implementation , this law not only guarantees air - to - ground missiles to ascent quickly , but also satisfies the requirements of midcourse phases . the studies have important theoretical meaning and great value of engineering application 为满足实际作战的要求,基于最优控制理论和奇异摄动方法,提出了一种可保证中远程空地导弹快速爬升到最优高度的中制导律.它由变系数最优爬升控制,最小能量巡航控制和最小能量下滑控制组成.为了减小爬升段控制对下滑段的影响,提出了一种新的控制逻辑.最后针对某型空地导弹进行了仿真.结果表明,该中制导律较好地满足了中远程空地导弹在中制导段的要求.本文的研究结果具有较好地工程参考价值