搜索资源列表
FSAE
- 斯图加特大学Fsae珍贵视频,详细分析了侧向力变化及其他操纵稳定性性能,能看到侧倾,俯仰,横摆三模态下的解耦控制-Stuttgart University Fsae precious video, a detailed analysis of changes in lateral force, and other manipulation of the stability of performance, can roll, pitch, yaw under three modal decoupl
FSAE
- 斯图加特大学Fsae珍贵视频,详细分析了侧向力变化及其他操纵稳定性性能,能看到侧倾,俯仰,横摆三模态下的解耦控制-Stuttgart University Fsae precious video, a detailed analysis of changes in lateral force, and other manipulation of the stability of performance, can roll, pitch, yaw under three modal decoupl
Flight_Attitude_Control_Simulation
- 用LabVIEW实现的“飞行姿态控制仿真”。内有vi:俯仰和滚转控制器、航向控制器、键按下增大、键盘操作、姿态角误差转换、阻尼器。还有9个显示vi和12个模型vi。 飞行控制的目的主要是通过控制飞行器的姿态和轨迹来完成飞行任务,然而飞行轨迹很大程度由飞行姿态决定。可见飞行器姿态控制,在整个飞行控制系统中处于重中之重的地位。飞行姿态控制的好坏直接关系到飞机能否安全、平稳、快速的地飞行。与其它控制系统一样,可用稳定性和动稳态性能来衡量控制效果。稳态时,要使飞行器姿态足够接近所需的飞行姿态,才
Strapdown
- 一、数据说明: 1:惯导系统为指北方位的捷连系统。初始经度为116.344695283度、纬度为39.975172度,高度h为30米。 初速度为v0=[0.000048637 0.000206947 0.007106781],飞行高度不变。 2:jlfw中为600秒的数据,陀螺仪和加速度计采样周期分别为为1/80秒和1/80秒。 3:初始姿态角为[0.120992605 0.010445947 91.637207](俯仰,横滚,航向,单位为度), jlfw中保存的为比力信
mega16
- mega16实现卡尔曼滤波计算俯仰角和横滚角程序-Kalman filter mega16 pitch angle and roll angle calculation program
3dtrans
- 3D Space Coordinate Transformations This folder contains 3 files (m-functions) : - t2x.m Transformation Matrix to Generalized Position Vector. - x2t.m Generalized Position Vector to Transformation Matrix. - m2m.m Mass/Inertia Tensor
digicom
- digital compass with honeywell sensors and roll pitch sensor multiplexer
DCM
- The direction cosine subrotines, which can be used to estimate roll and pitch using an IMU.
model_of_ship
- 逆合成孔径雷达仿真舰船图像,包括舰船的俯仰、滚动、偏航运动。-Inverse synthetic aperture radar image simulation of ship, including the ship' s pitch, roll, yaw movement.
EKF_MEMS
- 姿态信息是飞行控制中最关键的参数之一,因此姿态测量成为飞行控制系统首要解决的问题。利用多MEMS传感器研制了一种微型姿态测量系统。利用三轴MEMS加速度计和三轴MEMS陀螺数据,由方向余弦矩阵的姿态表示形式推导了扩展Kalman滤波方程,解算出飞行器的俯仰角和横滚角 设计专家系统判断飞行器的运动状态,并根据该状态调整滤波算法中的测量噪声矩阵,使系统可同时满足静态情况和动态情况的使用 利用空速和高度数据对俯仰角进行修正,利用GPS解算航向角。将实验结果与国外最新 的商用自动驾驶仪的姿态结果进行
6DOF-motion-platform
- 摘要:应用Matlab/Simulink对实验室研制的六自由度运动平台位置反解建模、仿真、分析,通过对上平台进行垂 荡、纵荡、横荡、纵摇、横摇和艏摇六个自由度方向上的运动仿真分析,得到了六个液压缸的长度变化规律,更直观的 了解了平台在不同运动情况下的运动规律 -Abstract: The six degrees of freedom motion platform location, Matlab/Simulink laboratory developed anti-solution mo
Ship_roll_-pitch_angle_simulation
- 船舶横摇纵摇角仿真程序,对船舶控制、导航解算等具有一定指导作用-Ship roll pitch angle simulation program
INS_Simulation
- 完整惯性导航解算,能够输出惯导解算出的东北天向速度和横滚、俯仰及偏航角。-Complete inertial navigation solver, able to output the INS the solution calculated Northeast days to speed and roll, pitch and yaw angle.
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
attdyn_DCM
- This program is written to compute the attitude angles roll-pitch and yaw through Direction Cosine Matrix Error dynamics.
error_model
- This program is written to compute the navigation position and sensor parameters as well as attitude angles roll-pitch and yaw through Si Error dynamics.
posdyn_llh
- This program is written to compute the position and angles roll-pitch and yaw through navigation system of Local-Level- coordinate system.
DMU_V0.7
- MPU9250,3轴运动传感器驱动,配合AHRS算法,可以计算出被测物体的横滚、俯仰、航线姿态,程序已经经过验证,可以放心使用!-MPU9250 3-axis motion sensor-driven, with the AHRS algorithm can calculate the object s roll, pitch, route profile, the program has been verified, you can be assured!
MPU6050-DMP
- 最近在学mpu6050 给大家分享下官方库 注意:roll pitch 角度变化正确 但是有点慢 而yaw有误差-最近在学mpu6050 给大家分享下官方库 注意:roll pitch 角度变化正确 但是有点慢 而yaw有误差
9轴融合算法mpu6050 hmc5883 kalmanfilter
- 卡尔曼滤波算法融合9轴传感器(MPU6050 + HMC5883 ) 的原始数据,给出准确的滚转、俯仰和偏航角度信息。(The Calman filtering algorithm combines the original data of 9 axis sensors (MPU6050 + HMC5883) and gives accurate information of roll, pitch and yaw angle.)