资源列表
ballistic_missile_inertial_navigation
- 弹道导弹从东经120北纬20高度30公里打目标东经150北纬30高度0的目标，关机点及飞行时间计算。还介绍了惯性导航的内容。 对于弹道式导弹：目标作为地球上的某一点，它是随地球一起在惯性空间运动的，因此需要迭代求解需要速度和自由飞行时间。按照给出的程序进行多次迭代解算即可得出考虑地球自转时的关机点参数解算和飞行时间计算。-20 ballistic missile from a high degree of north latitude and 120 east longitude hit tar
bieke
- 该程序通过建立二自由度汽车操纵动力学模型，实现对车辆操纵稳定性相关性能的仿真，程序中的Cf,Cr,lf,lr,m,u,Izz参数必须根据相关汽车参数赋值后才会正确运行，请应用者自行选用-The program through the establishment of two degrees of freedom vehicle handling dynamics model, to achieve the performance of the vehicle handling and stabi
Aircraft-Design
- 飞机设计手册+第4册+军用飞机总体设计.pdf-Aircraft Design Manual+ Chapter 4+ military aircraft design. Pdf
CNS
- 天文导航，弹道导弹SINS/CNS组合导航，轨迹发生器，卡尔曼滤波-Celestial navigation, ballistic missile SINS/CNS integrated navigation, trajectory generator, Kalman filtering
aircraft-6-DOF-simulation
- 飞行器六自由度建模，以及飞行器配平，线性化的matlab程序-The aircraft six degrees of freedom modeling, as well as aircraft trim, linearization matlab program
hough1
- 基于hough方法的航迹起始matlab算法-Track initiation method based hough matlab algorithm
Cable-stayed-bridgeModal-Analysis
- 此代码可作为分析一般斜拉桥模态分析的ANSYS源代码，类似情况更改几行代码即可。-This code can be used as general analysis of cable-stayed bridge modal analysis ANSYS source code, a similar situation to change a few lines of code.
SKYhook_suspension
- 悬架系统的天棚阻尼控制策略，有效减低系统的动载荷，加速度-Ceiling suspension system damping control strategy to effectively reduce the system dynamic loads, accelerations
SeismoSignal-v4.3.0_build101---
- 将加速度积分成速度位移，并且滤波，很好用-Displacement velocity integral of the acceleration and filtering, the good
norad
- TLE 卫星的双行轨道根数SGP/SGP4/SGP8/SDP4/SDP8模型函数及测试运行-Two Line Element
engine_model1
- 采用matlab平台下的simulink建立的发动机模型 帮助大家了解发动机的建模过程-Engine model using simulink matlab platform created to help people understand the modeling process engine
friction-velocity
- 计算PIV数据中湍流边界层内的壁面摩擦速度-Wall friction velocity within the turbulent boundary layer calculation PIV data