搜索资源列表
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
LanderMission
- 这个课题设计从地球的近地轨道起飞到达谷神星预定轨道并且着陆在其表面上的一种数值方法。基于有限时间的航行纠正点火而非瞬时推力数值计算和Matlab仿真。最后可以看到空间飞行器从地球的影响球飞到谷神星的影响球的飞行轨迹。-This project explores the mathematical methods and results of designing a mission to land a spacecraft on the asteroid Ceres by beginning in
LowThrust_Transfer
- 小推力航天器转移轨道程序，包括matlab源码和说明文档-Small thrust spacecraft transfer orbit procedures, including source and documentation matlab
Spacecraft_Control_Toolbox
- The Spacecraft Control Toolbox is composed of MATLAB m-fi les and mat-fi les, organized into a set of modules by subject. It is essentially a library of functions for analyzing spacecraft and missions. There is a substantial set of softwa
atmos_space_flight
- 大气层内航天器飞行动力学matlab仿真模型-The atmosphere inside the spacecraft flight dynamics matlab simulation model
TDAPR_oddyn
- The dynamics of orbit uncertainty in an unstable orbital environment are discussed with specific application to the orbit determination of a halo orbit about the Earth{Sun L1 point. This article documents a simplified orbit determination covari
kepler.m
- 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
SpaceFlightDynamics
- The ballistic category of atmospheric vehicles includes missiles, launch ve- hicles, and entry capsules. Some missiles and launch vehicles incorporate fi ns as aerodynamic stabilizing and control surfaces. The spacecraft are also catego-
Orbital_compute
- 进行航天器轨道运算经常用到的函数，包括坐标转换，经纬度转换，二体运动，轨道要素计算-For spacecraft orbit operations frequently used functions, including coordinate conversion, latitude and longitude conversion, two-body movement, and so calculated orbital elements
Infoagnosis
- 信息融合与多Agent技术在航天器能源管理系统在轨故障诊断中的应用-Information fusion and multi-Agent technology in energy management systems of spacecraft in-orbit failure diagnosis
TSdiction
- TSEOPM在轨航天器故障预报方法研究TSEOPM spacecraft in orbit Fault prediction-TSEOPM spacecraft in orbit Fault prediction
Spacecraft-orbit-extrapolation-code
- 航天器轨道外推代码（FORTRAN95/2003科学计算与工程，宋叶志），旨在介绍常微分方程处置问题的应用。-Spacecraft orbit extrapolation code (FORTRAN95/2003 scientific computing and engineering, Sung YE), aims to introduce the ordinary differential equation of the disposal of the application.
optimal_impulsive
- 最优脉冲轨道机动所需的圆形或椭圆形地球轨道的航天器。optimal impulsive maneuver required to de-orbit a spacecraft in a circular or elliptical Earth orbit-Round or oval Earth orbit spacecraft the optimal pulse orbital maneuvering required. optimal impulsive maneuver required to
guidaoxue
- 航天器轨道动力学与控制课件，1、2、3章-Spacecraft orbit dynamics and control courseware
guandaoquedingguidao
- 这是一条飞行器轨道转移的程序，利用惯性原理来控制轨道-This is a spacecraft orbit transfer procedures, the use of the principle of inertia to control track
atmospheric_descent
- 用于地月轨道返回航天器轨道仿真，包括仿真主程序和大气模型-Back for the Earth-Moon orbit spacecraft orbit simulation, including the main program and the atmospheric model simulation
orbit
- 计算航天器开普勒轨道方程，并画出其轨道图像-Kepler spacecraft orbit equation to calculate and draw its orbit image
lunwen
- 模拟 从地球发射飞船沿霍曼轨道到达金星并与之同步运动-Analog simulation emitted Earth orbit spacecraft reach Venus along Hohmann and synchronized motion
sc_attitude-master
- Goal of this project is to simulate the rotational motion of a spacecraft in orbit. Plots of Euler angles and polhode curves (angular velocity time histories) are generated. Equations of Motion included in this package are for a rigid body in a torqu
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