搜索资源列表
SINS-MatlabImplement
- 本程序是关于四元数法捷联惯导解算算法的matlab程序组合包，其中包括滤波初始对准仿真，罗经法初始对准仿真，捷联惯导解算仿真，组合卡尔曼滤波等演示程序及其必需的参数矩阵转换程序，程序算法皆是本人通过大量阅读捷联惯导经典论文书籍编写的，经过调试已经通过，所得圆锥误差，划桨误差与秦永元所编惯性导航一书相符，可靠性较高。适合惯导学习者参考改进使用 -This procedure is the law about quaternion SINS algorithm matlab solver co
hanjie
- 通过四元数和SOF对焊接的图像进行训练，从而使焊接的图形的边缘被保留，可以实现彩色图像的边缘提取-By quaternion and SOF welding training images, so that the weld edges are retained graphics, can achieve a color image edge detection
SINS
- 用四元数法进行姿态解算的matlab程序。-Quaternion method attitude algorithm matlab program.
jielian
- 惯性导航系统仿真算法程序，捷联惯导仿真程序，包含四元数更新，姿态角更新，速度位置更新等-Inertial navigation system simulation algorithm program, the strapdown inertial navigation simulation program, includes quaternion update, update attitude Angle, position update speed, etc
CHENGXU
- 基于四元数的空间贡献方程后方交会,基于四元数的脚锥体法空间后方交会,基于ola角的空间后方教会,三种算法对比,精度分析.mfc实现.有助于大家的学习.-Contribution equation based on quaternion space resection, foot cone method based on quaternion space resection, based on ola Angle of space behind the church, three algorith
psins151009
- 高精度捷联惯性导航系统Matlab工具箱：姿态向量、四元数、矩阵、滤波算法等各类子程序- High-precision inertial navigation system Matlab toolbox: attitude vector, quaternion, matrix, and other types of filtering algorithm subroutine
EXP1
- 四阶龙格-库塔，姿态角四元数更新算法，坐标系转换去除重力分量-Runge- Kutta attitude angle quaternion algorithm update
target_sat
- 本程序描述的是姿态四元数的积分求解过程，可用于航天航空以及机械领域。-This procedure is described in quaternion integral solution process can be used in aerospace and mechanical fields.
PSINS
- 工具箱主要功能: 1） 姿态向量、四元数、矩阵、滤波算法等各类子程序 2） 圆锥运动仿真 划船运动仿真 惯性器件随机误差仿真 3） Kalman滤波初始对准 基于惯性系初始对准 罗经法初始对准 大方位失准角EKF初始对准 大失准角UKF初始对准 速度+姿态传递对准 4） 纯惯性导航SINS仿真 航位推算、SINS/DR仿真 SINS/GPS组合仿真 GPS/BD/GLONASS单点伪距定位 SINS/GPS松/紧组合
hubulvbo
- 基于四元数互补滤波的四轴飞行器姿态解算算法。包括四元数、互补滤波、姿态结算-Solver algorithm based on quaternion complementary filter axis spacecraft attitude. Including quaternion complementary filter, posture settlement
qy136
- Including quaternion various calculations, Graduation useful Through repeated training lZApOFXlate have higher recognition rate.
用四元数为航天器设计的自适应滑模控制
- 使用姿态四元数为航天器姿态控制设计的自适应滑模控制器(Adaptive sliding mode control for spacecraft design using quaternion)