搜索资源列表
Mti
- 惯性测量组件Mti进行数据采集，利用陀螺和加速度计数据进行捷联姿态角解算，采用四元数更新算法，解算周期可调。
扩展卡尔曼滤波姿态解算-姿态融合
- 扩展卡尔曼滤波姿态解算，matlab程序，解算方法
sins
- 该程序包括了飞行器轨迹计算、陀螺和加速度计的采样输入、以及由四元素解算出的飞行器姿态、位置、速度-The program includes the aircraft trajectory calculation, the sampling gyro and accelerometer input, and the solution calculated by the four elements of aircraft attitude, position, velocity
imu_ahrs
- 基于IMU(三轴角速率、三轴加速计和三轴磁场)的方位姿态解算系统(ahrs)，基于C语言开发，VC 6.0编译器，可方便的移植到其他环境。-Based on the IMU (three-axis angular rate, three-axis accelerometer and three-axis magnetic field) to locate gesture Solution System (ahrs), based on C language development, VC 6.0
Navigation
- 利用比力、加速度信息解算出惯性导航所需的速度、位置和姿态信息-Than the use of force, acceleration of information required for inertial navigation solution to calculate the speed, position and attitude information
LAMBDA_CPP
- 在利用GPS载波相位整周模糊度解算载体姿态系统中，整周模糊度的算法实现—基于最小二乘估计调整方法-In the use of GPS carrier phase the whole week fuzzy degrees for calculating carrier phase integer ambiguity resolution based on the least squares estimate adjusting method
strapdown
- matlab实现捷联惯性导航解算，四元数更新姿态矩阵。-SINS solver matlab
SINS
- 用四元数法进行姿态解算的matlab程序。-Quaternion method attitude algorithm matlab program.
adis16405
- 根据ADIS16405进行姿态解算得到航向横摇纵摇-according to the ADIS16405 attitude solution obtained yaw roll pitch
Strapdown
- 捷联惯性导航算法完整版（单子样姿态解算算法）-Strapdown inertial system
DirectionCosin
- 载体的姿态解算算法是实现捷联式惯性导航系统精确导航的核心技术之一，采用了标准方向余弦法求解惯性导航的位置姿态-Carrier attitude algorithm of the algorithm is to achieve strapdown inertial navigation system is one of the core technology of accurate navigation, using the standard method of direction cosine
RotationVector
- 载体的姿态解算算法是实现捷联式惯性导航系统精确导航的核心技术之一，采用了标准旋转矢量法求解惯性导航的位置姿态-Carrier attitude algorithm of the algorithm is to achieve strapdown inertial navigation system is one of the core technology of accurate navigation, using the standard rotation vector method to s
Euler
- 载体的姿态解算算法是实现捷联式惯性导航系统精确导航的核心技术之一，采用了标准欧拉法求解惯性导航的位置姿态-Carrier attitude algorithm of the algorithm is to achieve strapdown inertial navigation system is one of the core technology of accurate navigation, using the standard eulerian method to solve the
MWC
- MWC飞控代码，可实现四轴飞行器空中姿态解算和运动控制。-MWC FM
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
imu_ahrs
- imu_arhs的程序：基于IMU(三轴角速率、三轴加速计和三轴磁场)的方位姿态解算系统(ahrs)，基于C语言开发，VC 6.0编译器，可方便的移植到其他环境 -imu_arhs program: Based on the IMU (three-axis angular rate, three-axis accelerometer and three-axis magnetic field) orientation attitude algorithm system (ahrs), bas
utlimate_ekf
- 多旋翼无人机使用扩展卡尔曼滤波的姿态解算算法仿真代码-Unmanned aerial vehicle (uav) attitude algorithm of extended kalman filtering algorithm simulation cod
zld2attitude
- 捷联惯导系统姿态解算，从IMU读入数据，输出数据与INS进行比对-Attitude Algorithm in Strap-down Inertial Navigation System
INS-Matlab-code
- 惯性导航的解算，附带速度、姿态、位置的姿态解算，内容很全(Inertial navigation solution, with speed, attitude, position of the attitude calculation, the content is very complete)
惯性导航精解算程序
- 惯性导航姿态解算，附带程序详解，内容完全可以直接使用(Inertial navigation attitude calculation, with detailed procedures, the content can be used directly)