搜索资源列表
rocket
- 导弹控制系统的鲁棒控制设计实例，包括3中不同的方法，有详细的注解和最后simulink 仿真。
Rocket
- 很好的高速口的设计资料，很好的高速口的设计资料 很好的高速口的设计资料-In design of large-scale access convergence router(hereafter referred to ACR) forwarding engine, the Xilinx Virtex-4 FPGA!s RocketI/O r multi-gigabit transceiver is used to satisfy the need of high speed and st
rocket
- 一个可爱的火箭上天 超赞 一个C实例-rocket c on the sky
rocket
- 一个六自由度火箭的鲁棒控制程序，该程序鲁棒H infinity control, robust loop shaping control 和mu analysis control三种不同的控制算法，并与火箭的非线性模型仿真结果进行了对比。-A six DOF robust control rocket program that robust H infinity control, robust loop shaping control and mu analysis control of th
Rungerkutta4
- 该程序利用4阶龙格库塔方法解二阶常微分方程，该微分方程描述火箭发射时质心运动轨迹。-The program uses the 4th order Runge-Kutta method of second order ordinary differential equations, differential equations describe the mass center when the rocket trajectory.
Rocket_plot
- Simply calculus for exhaust gases, altitude coast phase time, diameters for a required parachutes from a rocket.
rocket
- 导弹飞行器鲁棒控制器设计，其中包括H无穷和miu综合两种方法-Robust controller design for aircraft missiles, including H infinity and integrated two methods miu
recket
- for rocket engine calculation.-rocket calculation.
bulai
- for rocket engine calculation.-rocket calculation.
height
- 这段源程序是用来计算火箭发动机的高度特性。-to calculate the height of the rocket engine.
Missile--algorithms
- 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-Missile trajectory analysis algorithms, simulation of ballistic missiles to achieve two-stage rocket flight
rocket
- rocket source code matlab code
rocket
- 导弹六自由度的仿真，matlab编写，实现导弹飞行仿真-Six degrees of freedom missile simulation, matlab write to achieve the missile flight simulation
target-tracking-system-in-rocket
- 火箭系统的多目标跟踪的算法，对大家应该有帮助-Rocket system multi-target tracking algorithm, we should help
the-control-of-a-rocket
- 一个火箭轨道控制程序，利用模态综合法降阶后，对火箭发射过程的振动模态进行观测和控制-A rocket orbit control procedures, the use of reduced-order modal synthesis method, the process of rocket vibration mode for observation and control
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- 固体_液体火箭发动机环境下3DC_SiC喉衬烧蚀性能实验.-Solid _ liquid rocket engine environment 3DC_SiC Throat ablation performance test.
huojiandandaojisuan
- 计算火箭飞行的弹道。采用欧拉法，龙哥库塔近似计算火箭飞行弹道。-Calculation of the rocket flight trajectory. Using Euler method, Long Ge Kuta approximate rocket flight trajectory.
pressure-established
- 端面燃烧固体火箭发动机压强建立过程计算程序 输入为比热比，燃气气体常数，点火温度，推进剂密度，装药直径，喷管喉部直径，装药体积，燃速相关常数 输出为压强和工作时间-Face charge calculation of solid rocket motor process of establishing the working pressure Input for the specific heat ratio, gas gas constant, ignition temperature,
tube-charge-pressure-established
- 管型燃烧固体火箭发动机压强建立过程计算程序 输入为比热比，燃气气体常数，点火温度，推进剂密度，装药直径（内径和外径），喷管喉部直径，装药体积，燃速相关常数 输出为压强和工作时间-tube type of solid rocket motor combustion pressure build process calculation programs for heat input than, gas gas constant, the ignition temperature, propellan
missile-rocket
- 一个关于导弹，火箭的程序，里面有阻力系数等气动参数。-A missile, rocket program, which drag coefficient and other aerodynamic parameters.