搜索资源列表
飞船着陆
- 本源程序是模拟飞船着陆的游戏，有一定的趣味行~！-the source of the spacecraft landing simulation of the game, have a fun trip ~!
spacetools
- Spacecraft Engineering Toolbox Ver. 3.2
flysimulation
- 基于空间飞行器的姿态仿真源程序，仿真表明非常的准确。-Based on the spacecraft attitude simulation source code, simulation shows that very accurate.
2004_5337
- Particle Filtering for Sequential Spacecraft Attitude Estimation 卫星姿态估计的另外一种粒子滤波的介绍-Particle Filtering for Sequential Spacecraft Attitude Estimation for Satellite Attitude estimated another particle filter introduction
zairuzhidiandandao
- 用来计算航天器再入质点弹道，其中包括插值算法，龙格库塔法以及大气模型-Used to calculate the particle trajectory of spacecraft re-entry, including the interpolation algorithm, Runge-Kutta method as well as atmospheric model
SpacecraftAttitudeDynamicsanControl
- Spacecraft Attitude Dynamics and Control 航天器姿态控制的课件，十分难得；内容通俗易懂；十分完整；是从事航天研究的必须知识-Spacecraft Attitude Dynamics and Control of Spacecraft Attitude Control courseware, very rare the content of user-friendly very integrit
Spacecraft_Engineering_Toolbox
- Spacecraft Engineering Toolbox，这个工具箱很不错的-Spacecraft Engineering Toolbox, this Toolbox is very good
2007081312413982768
- 基于载波相位三差的航天器GPS/INS组合姿态算法-Based on carrier phase III spacecraft poor GPS/INS Attitude Algorithm portfolio
IDG300_system_design_information
- 二轴陀螺仪IDG300系统设计资料，可应用于空中鼠标定位，飞行器姿态校准等，该部分包含芯片的datasheet和温度补偿等方面的资料-B-axis gyroscope IDG300 system design information, can be applied to air mouse positioning, calibration, such as spacecraft attitude, which contains the
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 simplifie
Solar
- 用Directx3D开发的太阳系程序，实现了飞船在地球场景和太阳系场景的自由漫游，对于D3D的基础技术是个不错的总结-Directx3D development of the solar system with applications that implement the spacecraft in the Earth scenes and the freedom to roam the solar system scene, for
ApplicationoftheRunge2KuttaAlgorithminReal2time.ra
- _龙格_库塔_算法在航天器实时落点计算中的应用的文档。-_ Runge-Kutta _ _ real-time algorithm for spacecraft impact point calculation documents.
gmat-src-2008-09-30
- 用于航天器和卫星的任务分析的早期规划，戈达德航天中心研发，源代码开放-for spacecraft mission analysis
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
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 elemen
Flight_Attitude_Control_Simulation
- 用LabVIEW实现的“飞行姿态控制仿真”。内有vi：俯仰和滚转控制器、航向控制器、键按下增大、键盘操作、姿态角误差转换、阻尼器。还有9个显示vi和12个模型vi。 飞行控制的目的主要是通过控制飞行器的姿态和轨迹来完成飞行任务，然而飞行轨迹很大程度由飞行姿态决定。可见飞行器姿态控制，在整个飞行控制系统中处于重中之重的地位。飞行姿态控制的好坏直接关系到飞机能否安全、平稳、快速的地飞行。与其它控制系统一样，可用稳定性和动稳态性能来衡量
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
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 cove
Functional-behavior-of-the-spacecraft-GN_C-System-
- 航天器GN_C系统功能行为建模与仿真平台研究Functional behavior of the spacecraft GN_C System Modeling and Simulation Platform-Functional behavior of the spacecraft GN_C System Modeling and Simulation Platform
Integracecraft
- 航天器综合测试系统设计Integrated Test System for Spacecraft-Integrated Test System for Spacecraft