搜索资源列表
weixing.rar
- matlab实现的卫星轨道模拟，利用卫星轨道根数参量，通过求解开普勒方程求解卫星轨道模型,err
matlab.rar
- matlab实现的卫星轨道模拟，利用卫星轨道根数参量，通过求解开普勒方程求解卫星轨道模型,matlab implementation of satellite orbit simulation, the number of satellite orbit parameters, by solving the Kepler equation model of satellite orbit
sgp.rar
- NORAD公布的两行星历数据计算轨道参数模型，本程序包括SGP SGP4 模型,NORAD released two calendar data planet orbit-parameter model, the process includes the SGP SGP4 model
fortran
- 卫星轨道预测模型SGP的matlab源代码，经过了验证，可行！-SGP satellite orbit prediction model of the matlab source code, after verification, viable!
WSP
- 导弹轨道仿真源代码，模型可见钱杏芳《导弹飞行学》第二章的建模，采用四阶龙哥库塔仿真-Missile trajectory simulation source code, the model can be seen Qian Xing-fang, " Missile Flight Science," Chapter II of the modeling, simulation of a four-order Longge Kuta
SARorbitFitting
- 利用SAR卫星的已知的多个时刻的位置和速度信息，精确地拟合出SAR卫星的轨道模型。可用于计算出任意象元成像时刻卫星的位置-SAR satellites known to use multiple moments of position and velocity information, accurately fitted SAR satellite orbital model. Images can be used to calculate the yuan as the location of
spaceborne_SAR
- 1.本程序是自己刚刚接触SAR时编写的时域星载SAR点目标回波仿真，包含了卫星轨道模型、计算星目斜距时用到的各种坐标系转换、SAR回波计算模型以及简单的SAR成像模型，希望对初学者有所帮助。 2.相应的参考资料可查找《卫星轨道姿态动力学与控制》及《魏钟铨_合成孔径雷达卫星》；-1. This program is just contact with their own prepared when the time domain SAR spaceborne SAR point target
SAR-satellites
- 利用SAR卫星在多个时刻的位置和速度信息，计算出任意象元成像时刻卫星的位置，拟合出SAR卫星的轨道模型。-Using SAR satellite in multiple time position and velocity information to calculate as the image element imaging time satellite position, fitting the SAR satellite orbital model.
Satellite_-orbit
- 卫星轨道——模型、方法和应用配套程序,很经典的程序-satelliate orbit-models, methods and applications
GEODA
- 卫星轨道模型，预测卫星轨道，数值，以及轨道根数情况-Satellite orbit model, the satellite orbit prediction, numerical, and track the number of cases
RME_BEAM3
- 采用ANSYS建立的轨道模型，请有需要的人自行下载-The rail model was established by using BEAM3 element
spinning tether
- 基于Mathcad（也可转为matlab程序）的旋转系绳系统模型，以牛顿力学建模，考虑系绳弹性，可用于任意开普勒轨道建模仿真。(The Mathcad based model of the rotating tether system, which considers the tether elasticity, can be used for arbitrary Kepler orbit modeling and simulation.)
ECI_ECEF
- ECI与ECEF转换关系，卫星轨道模型方法，应用相关(ECI and ECEF conversion relation, satellite orbit model method, application correlation)
orbit
- 地月系统中，探月航天器运动的简单的数学模型，月球绕地运动近似为匀速圆周运动，程序中各天体坐标可以在JPL的星历表中查询修改。(In the Earth Moon system, the simple mathematical model of lunar exploration spacecraft motion is similar to the uniform motion around the moon. The coordinates of celestial bodies can be
目标追踪
- 导弹打击目标跟踪，轨道模型优化，算法优化等等。(Missile hitting target tracking, track model optimization, algorithm optimization and so on.)
火星转移轨道matlab仿真
- 以二体问题为模型，从地球发射航天器探索火星，途中需经过一次无动力金星借力，寻找最优（总速度增量最小）的发射时间窗口和飞行时间，并绘制地球到金星的Pork-Chop发射能量等高线图。发射时间窗口为2023—2033年，总飞行时间不得大于2年。(Taking the two body problem as the model to explore Mars from the earth, it is necessary to seek an unpowered Venus transit force
RPC_Orthorectification
- 对于高分辨率遥感卫星数据而言，目前几乎都提供了有理函数模型（RFM）来进行图像几何校正（SPOT系列提供了有理函数模型之外还提供了严格轨道模型）。对遥感影像进行校正目前最常用的就是使用有理函数模型来进行校正。(For high-resolution remote sensing satellite data, the Rational Function Model (RFM) is currently available for image geometry correction (the SP
J2
- 考虑地球扁率摄动，求解近地卫星轨道六根数，(Consider J2 perturbation to solve the number of six tracks)
iridium_ideal
- 铱星在stk软件中的场景建模包含66颗星6个轨道(iridium scenario model)
桥梁上CRTSⅠ型双块式无砟轨道模型命令流
- 在桥上建立长度为32m的crts2型双块式无砟轨道(Construction of crts2 double block ballastless track on Bridge)