搜索资源列表
PWM
- PWM 电机控制实验针对微型直流。两路带死区的 PWM 信号直接从 DSP 上产生，电机 驱动采用的是 4 个 PIN 三极管，可控制正反转。DSP 的 PWM 口在复位和无控制态度下为 IO 口，且为高电平，这样可能引起4个NPN管同时导通。为了防止这种情况的发生，DSP 出来的PWM信号进行了反向，即复位时给NPN基极的时低电平。 -PWM DC motor control experiment for the micro. Two PWM signals with dead
DSP_INS_1.0
- The open source project DSP_INS is an inertial navigation system on the TI DSP platform TMS320F28335 with MEMS inertial sensors and commercial GPS module. Inertial sensors are actually used only for estimating attitude, heading and velocity.
ADC_4PWM_3_Done
- DSP TMS320F2812的四轴飞行器控制程序，包含四路PWM输出，AD采集，及陀螺仪和加速度计的数据融合代码，姿态调整采样简单的PID控制算法-DSP TMS320F2812 four shaft vehicle control program, including four road PWM output, AD collection, and gyroscope and accelerometer data fusion code, attitude adjustment sampli
SCI_shuchubijiao_PWM_Done
- DSP TMS320F2812四轴单臂控制程序，包含姿态融合，串口调试上位机控制，能达到单臂稳定在设定角度的效果-DSP TMS320F2812 four shaft single arm control program, including attitude fusion, serial debugging PC control, can achieve stable arm in setting Angle effect
hf048
- It comprises aircraft flight attitude control, such as slip angle, tilt angle, roll angle, pitch angle, Including the least squares method, the SVM, neural networks, 1 _k neighbor method, Transceiver contains two client programs.
jhtut
- This function is used to calculate the arbitrary function of the first order partial derivative (numerical methods), It comprises aircraft flight attitude control, such as slip angle, tilt angle, roll angle, pitch angle, Prediction Error Method for P