搜索资源列表
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
single_sample
- 单子样等效圆锥矢量算法估计圆锥运动的姿态角。-List of equivalent cone-like vector algorithm estimated attitude angle cone movement.
dgao
- 飞行器纵向回路姿态控制系统中阶跃干扰时定高平飞-Aircraft vertical loop attitude control system in step interference Gaoping set to fly
VectorMatchingV01
- Attitude determination using vector matching
dongtai
- 捷联惯导的C程序实现，四元数表示姿态，动态数据显示，MATLAB进行图像处理，包含原始数据。-SINS of the C program implementation, said the attitude quaternion, dynamic data, MATLAB for image processing, including raw data.
jingtai
- 捷联惯惯性导航的C程序实现，四元数表示姿态，静态下进行试验，MATLAB进行图像处理，包含原始数据。-Strapdown inertial navigation of the C programs used to achieve, said the attitude quaternion, static tests under, MATLAB for image processing, including raw data.
xiaotuoluo
- 捷联惯导的C程序实现，四元数进行姿态更新，MATLAB进行图像处理，包含原始数据。-SINS of the C program implementation, quaternion for attitude update, MATLAB for image processing, including raw data.
coning-algorithm
- coning_atti:基于角速率输入的1～5子样等效转动矢量姿态仿真程序。 coning_atti_imu_error：等效转动矢量法仿真程序，包含1～4子样的各种等效转动矢量法，以读文件形式读取IMU输出参数，IMU参数由wnbb_error事先生成。 wnbb_error:用来产生带IMU误差的标准圆锥运动Gyro输出参数。 -coning_atti: Based on the input angular rate of 1 to 5 sub-sample rotat
MagneticSensor
- 地磁传感器文章，包括EMS地磁传感器、地磁导航技术及其应用、基于磁传感器MMC212的电子指南针、基于地磁原理的计转数传感器技术研究、水平定向钻进随钻姿态测量及误差补偿-Geomagnetic sensor article, including EMS magnetic sensors, magnetic navigation technology and its applications, based on magnetic sensor MMC212 electronic compass,
zitai
- 空间飞行器三轴稳定姿态动力学仿真，三轴稳定姿态动力学仿真-Stable attitude dynamics simulation of the space vehicle three weeks
helicopter-angle-PID
- 直升机的三个姿态角的pid控制算法，matlab中的simulink仿真程序，配合最优pid设计算法，得到很好的控制效果-Three attitude angle of the helicopter pid control algorithm matlab in simulink simulation program, with the optimal pid design algorithm, well controlled
Satellite-Attitude
- 卫星运动学和姿态动力学模型，采用Matlab的S-function来创建模型，可以方便更改参数-Satellite kinematics and attitude dynamics model using Matlab S-function to create the model, you can easily change the parameters
QuaternionRongekutta
- 求解陀螺仪的姿态角，采用四元素的四阶龙格库塔法求解。-Solving gyro attitude angle, using the four elements of the fourth-order Runge-Kutta method to solve.
fangxiangyuxian
- 姿态更新算法之一：方向余弦法,直接求解姿态矩阵微分方程-Attitude updating algorithm: direction cosine method, the direct matrix differential equation solving attitude
satellite_attitude_control
- 执行机构采用飞轮控制的卫星姿态控制系统仿真-attitude control system simulation of wheel controlled satellite
AttDet
- Toolbox for attitude determination with a multiple-antenna system using GPS
Kalman-matlab
- 传感器姿态解算 matlab工具箱全部程序自带测试文件程序-Sensor attitude algorithm matlab toolbox full program comes with the test documentation procedures
zongxiang
- 飞机纵向运动分析，包括高度、姿态等控制，在程序中可以自己选择控制模式-Aircraft longitudinal motion analysis, including altitude, attitude control, etc., in the program can choose the control mode
STM32XXX
- STM32多轴姿态程序代码，-Multi-axis attitude STM32 program code,
matlab-Attitude-adjustment
- matlab编写的四旋翼姿态调整模拟器，可用于上位机。-matlab prepared four-rotor attitude adjustment simulator can be used to host computer.