搜索资源列表
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控制效果。稳态时，要使飞行器姿态足够接近所需的飞行姿态，才
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
Spacecraft_Engineering_Toolbox
- Spacecraft Engineering Toolbox，这个工具箱很不错的-Spacecraft Engineering Toolbox, this Toolbox is very good
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
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 chip datasheet and temperature
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
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 D3D based technology is a goo
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 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
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
Simulation
- P_FUZZY_PID飞行器大角度机动控制物理仿真-Control of Spacecraft Large Angle Maneuvers P_FUZZY_PID Physical Simulation
spacecraft-code
- 一个航天器的动力学响应程序，采用模态价值分析准则和内平衡法则进行模型降阶。-Dynamic response of a spacecraft program, the use of value analysis mode within the balance guidelines and rules for model reduction.
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.
spacecraft-attitude-quaternion
- 对航天器的姿态以四元数的方法建立的仿真模型 。对航天器进行建模-The simulation model for spacecraft attitude quaternion method established. Spacecraft modeling
Four-axis-spacecraft
- 四轴飞行器姿态控制系统设计 四轴飞行器具有不稳定、非线性、强耦合等特性,姿态控制是四轴飞行器飞行控制系统的核心 通过分析四轴飞行器的飞行 原理,根据其数学模型和系统的功能要求,设计了四轴飞行器的姿态控制系统 该系统采用stm32系列32位处理器作为主控制器,使用 ADIS16355惯性测量单元等传感器用于姿态信息检测 系统基于模块化设计的思想,各传感器都使用数字接口进行数据交换,结构简 单 使用PID控制算法进行姿态角的闭环控制,实验结果表明,飞行器能较好的稳定在实验平台上,系统
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