Search - kepler

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[Other resource] KeplerOrbit DL : 0: 这是用于计算天文中的开普勒轨道元素的程序，用MAtlab编写的，欢迎使用哦。-This is used to calculate the astronomical elements Kepler track procedures used MAtlab prepared, Welcome oh.
Date : 2008-10-13 Size : 2.06kb User : 王超
[matlab] KeplerOrbit DL : 0: 这是用于计算天文中的开普勒轨道元素的程序，用MAtlab编写的，欢迎使用哦。-This is used to calculate the astronomical elements Kepler track procedures used MAtlab prepared, Welcome oh.
Date : 2025-07-15 Size : 2kb User : 王超
[matlab] kepler_equation DL : 0: Solving Kepler s Equation Using Newton s iterative Method
Date : 2025-07-15 Size : 1kb User : Nafiseh
[transportation applications] Orbit DL : 0: 卫星轨道机动仿真程序。包括轨道机动仿真、初轨计算、开普勒参数和PV值之间的转换等。-orbit mechanics
Date : 2025-07-15 Size : 462kb User : 刘涛
[Algorithm] SolveKeplerEquationforE DL : 0: 开普勒方程求解函数, 方便简单，空间飞行器轨道计算常用-Solve Kepler s Equation for E
Date : 2025-07-15 Size : 1kb User : 冯军华
[transportation applications] 20090826_kepler_solver DL : 0: 给出了采用牛顿法解超越方程，求解椭圆轨道及双曲线轨道开普勒方程中的偏近点角的源程序及例子；给出了解普适方程的函数及例子，是研究轨道理论中的重要函数，均基于matlab编程-Gives the solution of transcendental equation using Newton' s method, for solving elliptic orbit and the hyperbolic orbits Kepler equation Eccentric anomaly of the source code and examples universal equation are given to understand the function and examples, is to study the orbital theory of the important functions, are based on the matlab programming
Date : 2025-07-15 Size : 4kb User : 刘涛
[Linux-Unix] kepler DL : 0: 开普勒问题模拟，用不同的算法，可以画出相应的轨道-Kepler problems simulation code
Date : 2025-07-15 Size : 1kb User : Xiao
[matlab] matlab DL : 0: 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
Date : 2025-07-15 Size : 1kb User : 杨济军
[AI-NN-PR] kepler.m DL : 0: 实现探测器的轨道的开普勒描述，是一个很好的仿真程序-TO REALIZE THE ORBIT FOR SPACECRAFT IN KAPLER
Date : 2025-07-15 Size : 1kb User : 袁星
[matlab] kepler DL : 0: matlab求解kepler参数数学模型建立→MATLAB数值分析方法求解的-use matlab kepler
Date : 2025-07-15 Size : 1kb User : guo
[GPS develop] tle DL : 0: 根据卫星的位置和速度，求取实时卫星轨道的两行根数，即6个开普勒根数。计算结果精度很高。-The position and velocity of the satellite strike two lines of the real-time satellite orbit root number, six Kepler root number. Calculation results of high precision.
Date : 2025-07-15 Size : 1kb User : 小roach
[CSharp] the-three-laws-of-Keplers DL : 0: 可以实现开普勒三定律，只是要输入数据而已-The realization of the three laws of Kepler s
Date : 2025-07-15 Size : 25kb User : 488
[Windows Develop] KSolveKeplerEe DL : 0: 开普勒方程求解函数, 方便简单，，空间飞行器轨道计算常用 -Kepler equation solver function, convenient and simple, commonly used in space vehicle orbital calculations
Date : 2025-07-15 Size : 1kb User : bargain
[Mathimatics-Numerical algorithms] winna- DL : 0: 最优估计最有用的程序的新方法，对于新人学习有很大的帮助，请大家多多指教共同交流-Matable In order to improve the adaptation property of the system by making the best of the direction of distribution of radar measurement errors, a optimum estimation algorithm for Kepler orbit is proposed, which yields a maximum likelihood estimation of the Kepler orbit with multi-spatio-temporal state based on both the preprocessing of the small manoeuvring model and the determining of initial value parameter with two spatio-temporal state.
Date : 2025-07-15 Size : 192kb User : 蒋海旭
[ELanguage] mrac DL : 0: 自适应控制的简单程序，对于初学者有很大的帮助，大家共同学习，共同进步-In order to improve the adaptation property of the system by making the best of the direction of distribution of radar measurement errors, a optimum estimation algorithm for Kepler orbit is proposed, which yields a maximum likelihood estimation of the Kepler orbit with multi-spatio-temporal state based on both the preprocessing of the small manoeuvring model and the determining of initial value parameter with two spatio-temporal state.
Date : 2025-07-15 Size : 1kb User : 蒋海旭
[MPI] shuzhifenxi DL : 0: 数值分析，对于普通的编程实现一定的算法有很大的帮组，这是本人作业，服役偶偶程序计一定的解释-In order to improve the adaptation property of the system by making the best of the direction of distribution of radar measurement errors, a optimum estimation algorithm for Kepler orbit is proposed, which yields a maximum likelihood estimation of the Kepler orbit with multi-spatio-temporal state based on both the preprocessing of the small manoeuvring model and the determining of initial value parameter with two spatio-temporal state.
Date : 2025-07-15 Size : 21kb User : 蒋海旭
[Other] kepler-equaction-DG DL : 0: 数值计算方法！利用离散梯度法计算开普勒方程！理论扎实易懂，方便学习-Numerical methods! Kepler equation is calculated using the discrete gradient method! Theory of solid and easy to understand, easy to learn
Date : 2025-07-15 Size : 562kb User : hb
[matlab] kepler DL : 0: Codigo solucionar el problema de Kepler
Date : 2025-07-15 Size : 291kb User : rentov
[matlab] kepler DL : 0: 二体问题下，牛顿法解开普勒方程，包含圆，椭圆，双曲线，抛物线-This function uses Newton s method to solve Kepler s equation
Date : 2025-07-15 Size : 2kb User : 朱啸宇
[Other] Kepler DL : 0: This code is for solving the Kepler equation for elliptical orbit. This code gives the relation between the eccentric anomaly and mean anomaly for different eccentricities of the elliptical orbit.
Date : 2025-07-15 Size : 48kb User : Amar

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