搜索资源列表
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
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
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
strapdown
- 一篇确定捷联惯导初始姿态的专利文章，通过设置监控陀螺对其他三个陀螺进行测漂-A determined attitude SINS initial patent articles, by setting the monitor to the other three gyroscopes to measure gyro drift
AttDet_23_Oct_2008
- 利用gps多天线载波相位技术，确定姿态软件。-The use of multi-antenna gps carrier phase technology, attitude determination software.
IMUtracking
- IMU姿态跟踪，利用粒子滤波器实现，可用于机器人姿态确定-IMU orientation tracking algorithm using particle filter.
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
AttDet_16_3_2009
- GPS 多天线系统的姿态确定，matlab工具箱-A MATLAB toolbox for attitude determination with GPS multi-antenna systems
LunarAzEl
- 月球方位角与高度预测 针对月球车提出了一种基于天文观测的自主位置姿态确定方法。建立了利用天体敏感器测量得到的天体高度和方位作为观测信息的量测方程，并利用月球车运动的三阶常加速-Azimuth and highly predictive of the moon rover for astronomical observations is proposed based on the independent position and at
C_newtyle
- 航天工程用轨道卡尔曼滤波器，姿态确定传感器组合为轨道罗盘+磁强计，是当前组合中最为常见的，适合于小型卫星-Kalman filter with orbital spaceflight, the orbital attitude determination sensor combination compass+ magnetometers, is currently the most common combination is suita
C_newtyle
- 航天常用姿态确定敏感器组合，太阳敏感器+速率陀螺+轨道罗盘，具体数据含义请参考章仁为的<《卫星姿态控制》>-Spacecraft attitude determination sensors commonly used in combination, sun sensor+ rate gyro compass+ tracks, the meaning of specific data please refer to Chap
siyuanshu
- 捷联惯导 四元数法 进行导航姿态解算 程序内有详细注解-SINS quaternion attitude solver for navigation with detailed comments
hods
- 陀螺_星敏感器的微小卫星姿态确定方法determination methods-_ Gyro micro satellite star sensor attitude determination methods
AttDet
- 航天器姿态确定工具包,可利用CA码和L1载波进姿态确定 -attitude determinantion tool
S3-A-ADCS-1-5-ADCS
- Swisscube的姿态确定与控制系统，内容详细-The ADCS of Swisscube
attitude-determinati-
- 多GPS天线姿态确定程序，包括文件读取、单点定位、双差定位、坐标转换以及姿态确定等。-a MATLAB toolbox for determining the attitude of a rigid platform by means of multiple non-dedicated antennas using global positioning system is presented. The programs em