搜索资源列表
cizhumokuai
- 磁阻数据计算，用于三磁阻的计算和分析，测斜姿态角的应用，花钱买的，是个好东西，传给大家-spend some money ，this c is very useful to your stury，read carefully youwill get what whatyou wangt
airplane-attitude-angle
- 用matlab实现飞机飞行姿态仿真，三维，姿态角的描述，不需要实物 -a m ethodf orai rplanea ttitudea nglem easuermentis p roposed.Th e system is made叩of theodolites, cameras, computers and time control systems. The camera is placed on the theodolite, and can take airplane s pict
matlab-airplane
- 用matlab实现飞机飞行姿态仿真，三维，姿态角的描述，不需要实物-a m ethodf orai rplanea ttitudea nglem easuermentis p roposed.Th e system is made叩of theodolites, cameras, computers and time control systems. The camera is placed on the theodolite, and can take airplane s pictu
PF
- 粒子滤波的matlab程序，用于求解航向姿态角-Particle filter matlab program for solving course attitude angle
UKF
- UKF扩展卡尔曼滤波，求解舰船航向角、姿态角！-UKF extended Kalman filter to solve a ship heading angle, attitude angle!
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
PostureUpdate
- 四元数更新在matlab中的实现，包括采样、更新四元数、规范化、得到姿态角-Quaternion update
senario
- vc程序中建立stk场景，添加卫星，驱动卫星按照vc中指定的姿态角运动-vc programme to set up stk senario ,drive satllite attitude movement
e2qaq2e
- 用欧拉角表示的飞行器姿态运动学方程在大角度时会出现奇异现象,而采用四元数来 表示,则可以避免这个问题。因此,飞行器运动学方程都采用四元数来表示。而飞行器的控 制规律都采用欧拉角来表示,且欧拉角表示姿态角比起四元数更加形象,更易于被人理解, 所以,在飞行器控制系统仿真设计的时候,需要四元数与欧拉角之间的转换。给定1 个欧拉 角,对应1 个四元数,因而欧拉角到四元数之间这种一一对应的关系使得欧拉角到四元数的 转换比较容易。但是,1 个四元数通常有1 个或者2 个欧拉角与之对应,它
Rongekutta
- 求解陀螺仪的姿态角，采用四元素的四阶龙格库塔法求解，含姿态初始四元素的确定。-Solving gyro attitude angle, using the four elements of the fourth-order Runge-Kutta method to solve, including the initial four elements determined attitude.
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.
Satellite_orbit_design
- 现需要在高度为600~700KM范围内，回归周期为30天的太阳同步轨道上布置一颗L波段的合成孔径雷达卫星。 1. 请设计合适的轨道参数，并仿真对应轨道下一个运行周期内星下点轨迹图（纬度和经度两个图）； 2. 计算多普勒中心频率，多普勒调频率与纬度的关系图（设姿态角为0°，天线视角20°~60°，推荐35°）； 3. 按高斯投影方式，将星下点轨迹图投影到地图坐标上。-Now requires a height of 600 ~ 700KM range, return period
MPU6050_stm32
- stm32读取MPU6050加速度、角速度和姿态角-stm32 read MPU6050 acceleration, angular velocity and attitude angle
SINS
- 捷联惯导的程序，自己编写，通过俯仰角偏航角等来计算出动态和静态下的姿态角以及角速度，在导弹路径规划上有运用。-SINS program, their preparation, through the pitch angle to calculate the yaw angle under static and dynamic attitude angle and angular velocity of the missile path planning on using.
SLARK-AHRS
- 云雀（SLARK)AHRS姿态解码程序,将从串口获得的数据包解码成三个姿态角-The decoding of slark AHRS from URAT port!
jielian
- 惯性导航系统仿真算法程序，捷联惯导仿真程序，包含四元数更新，姿态角更新，速度位置更新等-Inertial navigation system simulation algorithm program, the strapdown inertial navigation simulation program, includes quaternion update, update attitude Angle, position update speed, etc
Madgwick
- 无人机姿态测量系统matlab程序，输入传感器数据，输出无人机的姿态角信息-UAV attitude measurement system matlab program
jielianguandao
- 惯性导航系统属于一种推算导航方式．即从一已知点的位置根据连续测得的运载体航向角和速度推算出其下一点的位置．因而可连续测出运动体的当前位置。惯性导航系统中的陀螺仪用来形成一个导航坐标系使加速度计的测量轴稳定在该坐标系中并给出航向和姿态角-Inertial navigation system is a dead reckoning navigation mode. That is from a given point according to the measured continuous carr
HMC-Cor-YJ
- K60为主控芯片，MPU6050解算三维姿态角，姿态解算采用DMP和四元素算法。并带有TFT液晶触摸屏以及蓝牙4.0的开发。-Use k60 as the main control MCU。MPU6050 solving three-dimensional attitude angle, attitude solver algorithm using DMP and the four elements. And with a TFT LCD touch screen and Bluetooth
apm2.5
- 基于apm2.5的飞行器姿态角计算及输出 以及 GPS 高度 经纬度输出 -Calculated based aircraft attitude angle and height of the output and GPS latitude and longitude of the output apm2.5