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MISSILETEST
- 一个导弹发射程序，可多视角观察-a missile launch procedures, Revisited
chuizhi
- 垂直发射弹道仿真程序(采用四元数法).matlab编写。-Vertical launch trajectory simulation program (using the quaternion method). Matlab prepared.
quaternion_in_missile_flight_simulation
- 论述了四元数法在垂直发射战术导弹和火箭子导弹的仿真中的应用.对反坦克导弹和舰空导弹飞行弹道仿真中的具体应用进行了方程推导、计算分析。 -Discusses the quaternion method in the vertical launching tactical missile and rocket missile sub-simulation. The anti-tank missiles and ship-to-air b
MISSILETEST
- 实现模拟导弹发射场景，实现多视角观察导弹运行弹道-Implementation scenarios simulated missile launch, multi-perspective on running ballistic missile
MinEnergeOrbit
- 可生成从任意点发射攻击全球任意点的一条最小能量弹道，并确定关机点参数。-Can generate a minimum energy trajectory launch attacks from any point to any point worldwide, and to determine the shutdown point parameters.
jisuandandaochengxu
- 某炮弹质量为20KG，直径120mm，出炮口是的初速为800m/s，初始发射角等于45°，试计算弹道。解答过程与程序详解-A shell quality is 20 kg, 120 mm in diameter, out of the muzzle velocity of 800 m/s, initial emission Angle is 45 °, try ballistic calculation. The solution pr
zhudongduan
- 该程序为三级火箭发射弹道的主动段程序，经过三次点火达到目标轨道。-The program is for the three rocket launchers‘ active segment ballistic program, after three ignition, the rocket achieves the target track.
Trajectory
- 输入导弹的基本发射条件，可模拟弹道的轨迹和最终的命中点-Enter the basic missile launch conditions can be simulated ballistic trajectory and final hits
chuguan
- 发射弹道出管段，一个主程序，两个function，一个绘图，(Launching trajectory)
neidandao1.2
- 武器垂直冷发射方式中，需要将武器弹射出发射筒，本程序涉及弹射内弹道、武器运动规律、装药设计等。(In the vertical cold firing mode of the weapon, it is necessary to catapult the weapon into the launching barrel. The program involves the interior ballistics of ejection,
Untitled
- 导弹一般采用“自控 + 自导”的制导体制，卫星侦察信息支持下的导弹打击海上移动目作战过程为: 解算卫星侦察信息，获得目标指示信息;将目标指示信息装订到导弹导引部，发射导弹; 导弹按照预先设定的轨道飞行，到达自控终点位置，末制导雷达开机; 末制导雷达覆盖目标，截获目标信号，对目标定位; 导弹对目标进行自动跟踪飞行，直到命中目标(The missile generally uses "self-control + homing&q