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龙格库塔姿态解算
- 采用龙格库塔法对陀螺采集的数据进行姿态解算
mimu
- 自己仿真的四元数法的龙格库塔的姿态解算matlab仿真-Their simulation method quaternion attitude Runge-Kutta solver matlab simulation
program_and_result
- 捷联惯导解算程序，由导航数据解算载体位置与姿态信息-SINS solver, the navigation data calculating the position and attitude information vector
another
- 复杂捷联惯导的另一种解算方法，包括解算位置、速率与姿态-Complex SINS another solution method, including calculating position, velocity and attitude
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
navi_test
- 用四元数法的捷联惯性导航姿态解算程序。可以快速准确得到数据。-With the quaternion method Inertial attitude solver. You can get fast and accurate data.
attitude
- 基于四级四阶龙格库塔算法的MEMS IMU数据的捷联姿态解算-SINS solve
Attitude-solving-operator-program
- 物体姿态解算算法子程序，包涵了各种在姿态解算仿真是需要用到的子程序，-The object attitude solution to calculate another way the program encompasses a variety of attitude solution simulation is the need to use a subroutine,
biaocheng
- 关于接连管道系统姿态解算的Matlab仿真，应用了四元数算法-Matlab simulation solver on a series of piping systems gesture, application of the quaternion algorithm
jlgen
- 一段关于捷联惯导系统姿态解算的Matlab仿真程序-Matlab simulation program solver paragraph on the attitude of SINS
jlsins
- 一段关于捷联惯导系统姿态解算的Matlab仿真程序,有关于误差的计算-Matlab simulation program solver paragraph on the attitude of SINS
xuanzhuanshiliang
- 惯性器件的旋转矢量姿态解算，三子样的旋转矢量，有真实数据-Rotation vector of inertial devices attitude solution
Navigation_3_1
- 惯性导航的姿态解算，四元数解算，导航定位解算等-Inertial navigation attitude algorithm, the Quaternion solution, such as navigation and position
Strapdown-inertial-navigation
- 一个简单的捷联姿态解算算法 GPS-INS惯导算法-A simple strapdown attitude solver algorithm GPS-INS inertial navigation algorithm
SINS-algorithm
- 运用四元数方法进行捷联惯性系统的姿态解算，并由加速度计的数据和陀螺的数据计算导航参数-The four element method for strapdown inertial navigation system of the attitude calculation, and the accelerometer and gyroscope data data computation of navigation parameters
地心惯性解算matlab
- 用matlab编写的地心惯性解算程序，输入为加速度和陀螺仪的角速度，包含卡尔曼滤波，以及姿态解算，可以自己加误差。
ode45_linmod
- 荣格库塔姿态阶段，应用于航天领域，可以进行运算得出正确的姿态(The Carl Jung Kutta attitude phase, applied to the aerospace field, can be computed to obtain the correct attitude)
SINS
- 捷联惯导算法、四元数算法姿态解算、误差补偿及仿真分析，matlab仿真程序(Attitude calculation of strapdown inertial navigation system algorithm based on Matlab)
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)
ecef+sins
- 代码1用于将位置经纬高信息转换为地心地固坐标系下xyz信息；代码2是捷联惯导算法代码，用于将加速度计和陀螺仪输出的信息进行解算得到位置、速度和姿态信息。(Code 1 is used to convert the location of warp and weft information into XYZ information in a geocentric coordinate system; code 2 is a strapdown inertial navigation algorit