搜索资源列表
fangchengzu_diershiqi
- matlab求取弹道仿真过程中第二时期第二阶段各点的数据-matlab strike the second period of the second phase of the trajectory simulation process data points
keshechengxu_diyishiqi
- 弹道仿真中用于将真实环境中的清醒映射到计算机中 实现实时化 经济化-Trajectory Simulation for sober in the real environment is mapped to the computer in real-time economy of
Aviation-course-design
- 西北工业大学电子信息学院，三专业，航空外弹道课程设计，包含实现代码及实验报告。-School of electronic information, Northwestern Polytechnical University, three professional, aviation trajectory of curriculum design, including implementation of code and test report.
Trajectory-program
- 质点外弹道程序设计，包含龙格库塔解算常微分方程组的程序，是一个简单、全面的程序-Trajectory program
trajectory
- 控制弹道程序，关于航行器弹道的控制程序，进行定深航行的仿真程序-The program of trajectory
Missile-trajectory-simulation
- 导弹铅垂平面内的无控段和载入段弹道仿真MATLAB源代码-Missile trajectory simulation
dandaojisuan
- 弹道计算。可以计算导弹六自由度的运动轨迹和-Ballistic calculation
daodan-dandao
- 反舰导弹和战术导弹的弹道仿真模型，能够给出导弹在铅垂平面和三维空间的飞行弹道-Anti-ship missiles and tactical ballistic missile simulation model, able to give the flight trajectory of the missile in the vertical plane and three-dimensional space
daodan-simulation
- 包含导弹飞行力学的课程讲义等内容，另外还包含一个导弹弹道的仿真模型。实现性能较好-Contains the the course handouts content of the missile flight mechanics also contains a simulation model of the missile trajectory. To achieve better performance
internal-ballistic
- 改程序为火炮内弹道程序，可以计算气体压力，速度等变化情况-Reform program for the Interior Ballistic program can calculate the gas pressure, speed changes
navi.test
- 导弹弹道分析算法，模拟实现两级火箭的弹道导弹飞行过程-failed to translate
interior-ballistic
- 底排弹内弹道计算程序,使用VB编制，带有计算结果及附图可供参考-Interior Ballistic Caculate
guidance-law
- 比例导引法的导弹和目标之间，理想弹道模型，用于了解导弹和目前在最佳时间遭遇的图形-Proportional guidance law between missile and target, the ideal trajectory model, used to understand graphical missile and is currently experiencing in the best time.
ceshecheng
- 导弹参数已知的情况下，给定弹道倾角测射程-Ballistic missile parameters are known in the case of a given angle measurement range
waidandao_neidandao
- 从导弹外弹道到导弹内弹道的比较完整的编程实现-From external ballistics to the interior ballistics of complete programming
kongzhidandaoqingjiao
- 导弹结构参数给定，控制导弹弹道倾角的编程方案-The missile structure parameters given control solution for programming of the missile trajectory inclination
p
- 使用四阶龙格库塔法求解内弹道方程，得出二级轻气炮各项参数-Fourth-order Runge-Kutta method to solve ballistic equations, draw the two-stage light gas gun, the parameters of the
LGB
- 导弹理想弹道三维仿真，采用龙哥库塔法，攻击方式为纯追踪，对地攻击。-Missile ideal trajectory three-dimensional simulation, the use of the Long Ge Kuta law, attack pure pursuit, ground attack.
0
- 成功运用matlab语言编写的采用最流行的维普法优化飞行弹道的设计程序-Successful use of matlab language of the most popular [Optimization of the flight trajectory design process
bilidaoyinfa
- 比例导引法的几个matlab程序，根据绝对弹道进行编程设计-Proportional navigation law matlab program, according to the absolute ballistic Programming