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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
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
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.
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
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
RobotSimulate
- 给定机器人臂长和关节角度,确定机器人在空间中的位置和姿态.-Given the robot arm length and joint angles to determine the position of the robot in space and orientation.
the-face-detection-technique
- 人脸检测是指对于任意一副给定的图像，采用一定的策略对其进行搜索以确定其中是否含有人脸，如果是则返回一脸的位置、大小和姿态。-Face detection is a means for any one given image, the use of a certain strategy to search for it to determine whether it contains a human face, and if so return look the location, size, a
Rongekutta
- 求解陀螺仪的姿态角，采用四元素的四阶龙格库塔法求解，含姿态初始四元素的确定。-Solving gyro attitude angle, using the four elements of the fourth-order Runge-Kutta method to solve, including the initial four elements determined attitude.
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 embedded in this toolbox cover t
KF
- 初始对准是捷联惯导系统进行导航的前提，初始对准的好坏将直接影响到系统的导航精度。捷联惯导系统(SINS)初始对准的本质是确定载体的初始姿态。-The initial alignment of strapdown inertial navigation system is the premise for navigation, initial alignment will directly affect the quality of the navigation system precision.
6DOF platform
- 通过6各参数确定平台结构，输入六自由度平台缸长，正解计算平台姿态(Input six degree of freedom platform parameters, positive solution to calculate platform attitude)
INSNEW
- 根据给定的数据进行惯性导航的解算，从而确定姿态，速度和位置的更新(The calculation of inertial navigation based on the given data to determine the update of attitude, speed and position)
73881202
- 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()