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satellite1
- 针对卫星姿态控制中的一些常见运算的源码。如，四元素与欧拉角的互换，矩阵之间的运算等-against satellite attitude control of the operation some common source. For example, four elements and Euler angle swap between the matrix, etc.
gyro_EKF
- 给出了一种基于陀螺和四元数的EKF卫星姿态确定算法，非常实用-is based on a gyroscope and quaternion the EKF satellite attitude determination algorithm, a very practical
BasedOnMarginalizedPaticleFilteringSatelliteAttitu
- 基于Marginalized粒子滤波的卫星姿态估计算法。介绍了一种基于粒子滤波的全新的卫星姿态确定的算法，非常有借鉴意义
SAfilteringmethod
- 卫星姿态确定及敏感器误差修正的滤波算法研究。介绍了几种不同的滤波算法，如卡尔曼滤波，扩展卡尔曼滤波，粒子滤波等在姿态确定上的应用，并比较了它们仿真的结果
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
基于PWM的卫星喷气姿态控制系统
- 基于刚体三轴稳定对地定向航天器的PD+PWM姿态稳定与机动仿真。在原点小偏差线性化后，经过简单计算和调试，最后确定：Kp = [700 700 900],Kd = [2330 2400 3030]，姿态运动学和姿态动力学均由m文件编写，其余由simulink基本模块搭成。压缩包里的其他文件包括PWM的测试、触发器测试和内嵌m文件。主程序为kinematics.mdl
satellite1
- 针对卫星姿态控制中的一些常见运算的源码。如，四元素与欧拉角的互换，矩阵之间的运算等-against satellite attitude control of the operation some common source. For example, four elements and Euler angle swap between the matrix, etc.
gyro_EKF
- 给出了一种基于陀螺和四元数的EKF卫星姿态确定算法，非常实用-is based on a gyroscope and quaternion the EKF satellite attitude determination algorithm, a very practical
BasedOnMarginalizedPaticleFilteringSatelliteAttitu
- 基于Marginalized粒子滤波的卫星姿态估计算法。介绍了一种基于粒子滤波的全新的卫星姿态确定的算法，非常有借鉴意义-Marginalized particle filter based on the satellite attitude estimation algorithm. This paper presents a particle filter based on new satellite attitude determ
SAfilteringmethod
- 卫星姿态确定及敏感器误差修正的滤波算法研究。介绍了几种不同的滤波算法，如卡尔曼滤波，扩展卡尔曼滤波，粒子滤波等在姿态确定上的应用，并比较了它们仿真的结果-Satellite attitude determination and sensor error correction filtering algorithms. Introduced several different filtering algorithms, such as K
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
satelite
- 通过卫星的测量方程和状态方程来求解卫星的姿态。包括四元数，角度，角速度等等。-By satellite measurements to solve equations and state equations of satellite attitude. Including the quaternion, angle, angular velocity and so on.
STKtest1
- STK模拟卫星发射过程，通过文件驱动卫星姿态轨道数据。-STK analog satellite launch process, through document-driven satellite attitude orbital data.
VerilogHDL_tuxiang
- 介绍一种用于卫星姿态测量的CMOS图像敏感器--STAR250的时序驱动信号，并使用Verilog HDL语言设计驱动时序电路。经布线、仿真、测试后验证了驱动信号的正确性。 -Introduce a measurement for the satellite attitude CMOS image sensor- STAR250 timing drive signals, and use the Verilog HDL language
201003tecplot
- 简介卫星姿态控制系统的模型，并针对该模型分析故障发生的特点，故 障诊断的难点，以及可能发生故障的部位和故障的类型，给出故障检测的方法。-Introduction of satellite attitude control system model and the model for the analysis of the characteristics of faults, fault diagnosis of the diffic
EKF
- 卫星姿态确定的卡尔曼滤波，使用matlab 仿真的姿态确定-satellite attitude determination
姿态控制仿真
- 关于卫星姿态动力学的建模和姿态控制仿真，在code文件中(On the modeling and attitude control simulation of satellite attitude dynamics, in the code file)
仿真
- 基于极点配置实现卫星姿态角控制，有仿真和源代码(Satellite attitude angle control based on pole placement with simulation and source code)
SatNoControlSim
- simulink搭建的卫星姿态动力学仿真，参考书籍是章仁为的卫星轨道姿态动力学仿真，想学对卫星姿态有兴趣的同学强烈推荐(For the satellite attitude dynamics simulation built by Simulink, the reference book is Zhang Renwei's satellite orbit attitude dynamics simulation, which is hi