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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
Matlabtoolbox_space
- Matlab航天器工具箱，用于轨道计算，2D或3D的平面显示，包含计算多卫星轨道动力学模型和地面覆盖分析等-Matlab toolbox spacecraft for orbit calculation, 2D or 3D graphic display, including the calculation of multi-satellite orbital dynamics analysis model and floor coverings
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!
Orbitmodel
- 飞行器轨道仿真模型，参照飞行器教科书建模-Aircraft 6-DOF simulation model, refer to the textbook model aircraft
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
transrail
- 城市轨道交通客流需求预测模型，非集计思路-Urban rail transport passenger demand forecasting model, non-collection design ideas
exci
- 该函数exci（）在matlab中编写完成，实现的功能：将频域的轨道不平顺转换为时域的轨道不平顺激励，可以在仿真时作为Simulink模型的激励源输入。-This function can be used to source for rail excitations while simulating a simulink model.
rail_excitation
- 包括simulink程序与轨道不平顺美国谱的时域生成程序（m语言编写的函数），直接可用于matlab的simulink模型仿真，不用做任何处理。下载该压缩包，打开其中的rail_excitation.mdl，双击即可看到时域轨道谱生成-Simulink program including the United States and track irregularity spectrum time domain generation program (m language function), c
Modeling-of-trajectory
- Matlab进行再入式飞行器轨道建模与仿真，建立各种模型，最后获得飞行器的动力学模型，并调用龙格库塔函数求解该微分方程初值问题。-Matlab for reentry spacecraft orbit modeling and simulation, the establishment of various models, and finally obtain the dynamic model of the aircraft, and call the Runge-Kutta function
matlab-SGP4
- SGP4航天器轨道预报模型的MATLAB程序，可直接使用并对其进行二次开发。-Matlab program of SGP4 model for orbit prediction of spacecrafts.
chelunzukang
- 建立轨道车辆的简化模型，计算出车轮的阻抗，进而计算出轮轨作用力，用来研究车辆的振动特性-impedance of wheel
rowflying
- 串行编队卫星构形可观测性分析数值仿真程序，内建有二体轨道动力学模型，加入J2项摄动，并且使用了非线性EKF滤波算法。-Extended kalman filter was exploited to simulate the rowflying formation,J2 purtabation was taken into consideration
Genetic-Algorithm
- 遗传算法（Genetic Algorithm）是模拟达尔文生物进化论的自然选择和遗传学机理的生物进化过程的计算模型，是一种通过模拟自然进化过程搜索最优解的方法。遗传算法可以解决多种优化问题，如：TSP问题、生产调度问题、轨道优化问题等，在现代优化算法中占据了重要的地位，本例使用遗传算法求解最优解。-Genetic Algorithm (Genetic Algorithm) is a simulation of Darwinian natural selection and genetic mec
banqie_v70
- 已经调试成功.内含m文件，可直接运行，包含CV、CA、Single、当前、恒转弯速率、转弯模型，包括轨道机动仿真、初轨计算。- Has been successful debugging. M contains files can be directly run, It contains CV, CA, Single, current, constant turn rate, turning model, Including orbital maneuvering simulation, ini
foufing_v12
- matlab实现了五类灰色关联度模型的计算,包括轨道机动仿真、初轨计算,包括单边带、双边带、载波抑制及四倍频。- matlab implements five gray correlation degree computing model, Including orbital maneuvering simulation, initial orbit calculation, Including single sideband, double sideband, suppressed carri
moukai_v77
- 计算时间和二维直方图,本科毕设要求参见标准测试模型，包括轨道机动仿真、初轨计算。- Computing time and two-dimensional histogram, Undergraduate complete set requirements refer to the standard test models, Including orbital maneuvering simulation, initial orbit calculation.
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
卫星仿真
- 卫星二体轨道动力学模型仿真，用于卫星轨道模拟，航天领域(Satellite two-body orbit dynamics model simulation)