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Description: 该系统使用极其简便，即使 你对各种网络模型不是很深刻的了解，也可以很好的使用该系统。使用时， 你可以自己修改网络的各种参数，交互性较好，而且该系统通过大量的图示 及参数设置，可以让你了解每个应用实例实现的过程及详细步骤。-The system is extremely easy to use, even if you have to various network model is not very profound understanding can be a good use of the system. When used, you can change the network's own parameters, interactive better, but the system through a lot of icon and parameter settings, so you can understand each application process and the realization of detailed steps.
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Size: 534528 |
Author: 权威 |
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Description: 一个好用的模型参考自适应速度估计模型，已经经过测试-A useful model reference adaptive speed estimation model has been tested
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Size: 6144 |
Author: tata |
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Description: a small procedure attempting to read the mars data and for rock extraction.
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Size: 3878912 |
Author: 岳宗玉 |
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Description: 三相异步电机无速度传感器的matlab实现，采用的转速辨识算法为mars
matlab版本7.4-Three-phase induction motor speed sensorless matlab the realization of the speed identification algorithm used for the mars matlab version 7.4
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Size: 32768 |
Author: 江明 |
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Description: this is a project for mras with matlab 7
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Size: 13312 |
Author: m |
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Description: 本程序模拟了火星、金星、水星等行星相对地球的运动轨迹，对于研究行星运动规律极有帮助。-This procedure simulated Mars, Venus, Mercury and other planets relative to Earth' s trajectory for the study of the law of planetary motion very helpful.
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Size: 1024 |
Author: 凌凌漆 |
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Description: 基于MARS的无速度传感器矢量控制系统研究-MARS-based speed sensorless vector control system
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Size: 1471488 |
Author: caojianyang |
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Description: 基于MARS的PMSM无速度传感器矢量控制系统研究-MARS-based speed sensorless PMSM vector control system
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Size: 453632 |
Author: caojianyang |
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Description: 基于MARS的PMSM无速度传感器矢量控制系统研究-MARS-based speed sensorless PMSM vector control system
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Size: 4748288 |
Author: caojianyang |
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Description: 应用matlab语言，应用lambert变轨实现地球到火星的发射窗口的轨道寻优。内涵lambert变轨功能，星历计算等多个函数文件-Application of matlab language, application lambert achieve orbit the Earth to orbit Mars launch window optimization. Connotation lambert orbit function, ephemeris calculations and other functions file
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Size: 18432 |
Author: zhangyang |
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Description: 案例为运用最有控制原理，实现对火星探测器小推力变轨的控制实现。应用matlab仿真实现-Case for the use of the most control theory, to achieve the low-thrust orbit Mars probe control implementation. Application of matlab simulation
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Size: 3072 |
Author: 吴鹏 |
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Description: 上学学习matlab的期末考试试题：包括地球和火星绕太阳运转动画演示；利用两种不同途径求解边值问题；多种方法求解Lorenz模型；多种方法求解Apollo卫星的运动轨迹；利用Matlab设计一个简单的计算器，要求：（1）友好的交互界面；（2）至少能够实现加减与乘除预算。-School learning matlab final exam questions include: Earth and Mars around the sun animation using two different approaches for solving boundary value problem variety of methods to solve the Lorenz model variety of methods to solve the trajectory of Apollo satellites using Matlab to design a simple The calculator requirements: (1) friendly interface (2) addition and subtraction and multiplication and division to achieve at least the budget.
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Size: 358400 |
Author: 宋兵 |
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Description: 火星探测器最优小推力变轨MATLAB程序-Optimal low-thrust orbit Mars probe
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Size: 86016 |
Author: 刘延杰 |
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Description: 最优控制，火星探测器小推力变轨，可显示逃逸速度(Optimal control, Mars low thrust orbit transfer, can display the escape velocity)
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Size: 2048 |
Author: 松鼠38号
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Description: 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 on the way to find the optimal time window and time of flight (the minimum total velocity increment), and draw the contour map of the Pork-Chop emission energy of the earth to Venus. The total launch time window is from 2023 to 2033, and the total flight time is not more than 2 years.)
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Size: 14336 |
Author: 卓K |
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Description: This is a simulation code of orbital mechanics. We simulated the earth's orbit to Mars, and caught the gravity of Venus once, and achieved good results.
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Size: 1216512 |
Author: bhead |
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Description: 从地球到火星的模拟轨道运算及以燃料消耗为目的的优化。(Orbit simulation and optimization from earth to Mars.)
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Size: 13734912 |
Author: kkhahaha |
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