搜索资源列表
生活者姿态整站程序
- 生活者姿态整站程序 生活者姿态整站程序-Life posture whole lives were at stations throughout posture stations Life entire posture stations Life posture whole lives were at stations throughout posture stations
satellite1
- 针对卫星姿态控制中的一些常见运算的源码。如，四元素与欧拉角的互换，矩阵之间的运算等-against satellite attitude control of the operation some common source. For example, four elements and Euler angle swap between the matrix, etc.
weizijisuan
- 根据GPS回传的数据，进行坐标变换，计算应该达到的姿态-Return GPS data, coordinate transformation, the calculation should reach posture
clear
- 该原代码包括捷联惯导姿态程序,位置程序以及初始对准程序,实用性强,便于学习.
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。
velocitymatchsimulation
- 惯性导航的传递对准程序，一种速度加姿态的对准。
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
C_newtyle
- 航天工程用轨道卡尔曼滤波器，姿态确定传感器组合为轨道罗盘+磁强计，是当前组合中最为常见的，适合于小型卫星-Kalman filter with orbital spaceflight, the orbital attitude determination sensor combination compass+ magnetometers, is currently the most common combination is suitable for small satellites
trajection
- 用Matlab编写的轨迹发生器，输入初始的位置速度，姿态角，姿态变化等信息，模拟得到陀螺仪输出和加速度计的输出-Written with the Matlab path generator, enter the initial position, velocity, attitude, attitude changes and other information, the simulated gyro output and the output of the accelerometer
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
attref
- 在磁力计、重力加速度、机体加速度计模型基础上计算姿态角参数-In the magnetometer, gravity, body accelerometer attitude angle calculated based on the model parameters
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
openpilot_ahrs
- openpilot自动驾驶仪的姿态参考系统（AHRS）源码-openpilot Autopilot Attitude Reference System (AHRS) source
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
Floatboos
- 基于、的特征提取方法, 研究、算法的多角度分类器设计问 题在对图像进行主成分分析和独立成分分析后, 针对多姿态角目标识别问题, 提出了角度优先粗分 类的设计方法, 并给出系统流程, 最后-Based, feature extraction methods, research, multi-angle algorithms classifier design problem in the image principal component analysis and independent
PID
- 航天器姿态控制PID控制仿真程序，加入干扰值。-PID control of spacecraft attitude control simulation program, by adding the value of interference.
homeword2-06
- Matlab源码，仿真飞机姿态更新，主要是捷联惯导的姿态更新-Matlab source code, simulation of aircraft attitude update, mainly SINS attitude update
satellite_orbit
- 卫星轨道方面的知识，卫星轨道姿态动力学与控制-Knowledge of satellite orbit, the satellite attitude and orbit dynamics and control
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)