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daohangsuanfalunwen
- 本人平时收集的惯性导航算法的论文，对搞导航算法的人很有帮助。 1.易于实现的捷联式惯性导航系统仿真.pdf 2.测量运动物体姿态的三自由度定位算法的研究.pdf 3.基于MEMS 技术的微型惯性测量组合.pdf 4.基于四元数的空间全方位算法研究.pdf 5.捷联惯导积分算法设计（连载二）下篇：速度和位置算.pdf 6.数字磁罗经系统的设计.pdf 7.四阶龙格—库塔法在捷联惯导系统姿态解算中的应用.pdf
naviga090205.rar
- 捷联惯性导航的仿真程序用四元数法的捷联惯性导航姿态解算程序资源大小:...用四元数法进行姿态解算的matlab程序,Strapdown inertial navigation simulation program
flight
- OpenPilot开源代码，这个文件是其核心，包括飞控和姿态解算，网上也可以找到，但是得费点时间-OpenPilot of open source code, this file is its core, including flight control and attitude solving algorithm, on the net also can be found, but have to take some time
ArduIMU_1.9.8
- Arduino上开发的IMU小程序，对于姿态解算和数据融合的理解有一定帮助-Program for Arduino IMU developing
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
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
Fourth-order-dragon-Kutta
- 文介绍了利用四阶龙格-库塔法解微分方程的姿态解算方法，并以典型圆锥运动作为输入，检验了算法的可靠性。-The article introduced the use fourth-order dragon standard- Kutta law solution differential equation s posture resolving method, and takes the input by the typical conical motion, examined the algor
Fourth-order-Runge---Kutta-
- 四阶龙格-库塔算法在姿态解算中的应用,是实现圆锥运动的姿态解算。当旋转角速率w为定值的时候，我用龙格-库塔算法很容易解出了姿态矩阵四元数。-Fourth order Runge- Kutta algorithm of attitude algorithm.
gpsins
- 姿态解算程序，用于捷联惯导系统的姿态解析算法-Attitude solution procedures for the sins of attitude analytic method
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
the-fourth-order-Runge-Kutta
- 运用四元数推导，四阶龙格库塔发捷联惯导姿态解算，-The use of quaternion derivation of the fourth-order Runge Kutta hair SINS attitude solution,
open-head-tracker.src.0.1
- 本项目旨在制作一个用于第一人称视角(FPV)遥控飞行的头部姿态追踪系统。系统利用惯性测量单元测量头部运动姿态，生成相应的舵机驱动信号，利用遥控发射器传输到遥控飞机，驱动摄像云台跟随头部运动，达到模拟第一人称飞行的目的。 系统采用ATmega328 MCU；利用 BMA180 三轴加速度传感器、ITG3200 三轴角速度传感器、HMC5883 三轴磁场传感器组成 9 自由度测量单元；通过 1602 LCD 直观显示控制菜单。系统软件基于 Arduino，采用方向余弦矩阵 (DCM) 进行
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
20697951another
- 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 the strapdown inertial navigation of another kind of calculating method, including calculating the position, velocity and 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)
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