Eigen Revision
Dependencies: mbed LPS25HB_I2C LSM9DS1 PIDcontroller Autopilot_Eigen LoopTicker GPSUBX_UART_Eigen SBUS_without_mainfile MedianFilter Eigen UsaPack solaESKF_Eigen Vector3 CalibrateMagneto FastPWM
setup.cpp
- Committer:
- NaotoMorita
- Date:
- 2021-06-22
- Revision:
- 65:ea184054e659
- Parent:
- 61:c05353850017
- Child:
- 68:b9f6938fab9d
File content as of revision 65:ea184054e659:
#include "global.hpp" void setup() { pitchPID.setSetPoint(0.0); pitchratePID.setSetPoint(0.0); pitchPID.setBias(0.0); pitchratePID.setBias(0.0); pitchPID.setOutputLimits(-1.0,1.0); pitchratePID.setOutputLimits(-1.0,1.0); pitchPID.setInputLimits(-M_PI, M_PI); pitchratePID.setInputLimits(-M_PI, M_PI); elevServo.period_us(15000.0); elevServo.pulsewidth_us(1500.0); rudServo.period_us(15000.0); rudServo.pulsewidth_us(1500.0); accelgyro.initialize(); //加速度計のフルスケールレンジを設定 accelgyro.setFullScaleAccelRange(ACCEL_FSR); //角速度計のフルスケールレンジを設定 accelgyro.setFullScaleGyroRange(GYRO_FSR); //MPU6050のLPFを設定 accelgyro.setDLPFMode(MPU6050_LPF); //地磁気 mag_sensor.enable(); } void calibrate() { pc.serial.printf("\r\nEnter to Calibration Mode\r\n"); wait(5); pc.serial.printf("Acc and Gyro Calibration Start\r\n"); int gxs = 0; int gys = 0; int gzs = 0; int iter_n = 10000; for(int i = 0;i<iter_n ;i++) { accelgyro.getMotion6(&ay, &ax, &az, &gy, &gx, &gz); gxs += gx; gys += gy; gzs -= gz; //wait(0.01); } gxs = gxs /iter_n; gys = gys /iter_n; gzs = gzs /iter_n; agoffset[3] = gxs; agoffset[4] = gys; agoffset[5] = gzs; pc.serial.printf("Gyrooffset : 0, 0, 0, %d, %d, %d \r\n",gxs,gys,gzs); pc.serial.printf("Initial Magbias (Min) : %f, %f, %f\r\n", magbiasMin[0], magbiasMin[1], magbiasMin[2]); pc.serial.printf("Initial Magbias (Max) : %f, %f, %f\r\n", magbiasMax[0], magbiasMax[1], magbiasMax[2]); pc.serial.printf("Mag Calibration Start\r\n"); float inputMag[3]; float outputMag[3]; while(1) { mag_sensor.getAxis(mdata); // flush the magnetmeter inputMag[0] = mdata.x; inputMag[1] = mdata.y; inputMag[2] = mdata.z; magCalibrator.run(inputMag,outputMag); if(userButton.read() == 1) { break; } wait(0.001); } magCalibrator.getExtremes(magbiasMin,magbiasMax); pc.serial.printf("Magbias (Min) : %f, %f, %f\r\n", magbiasMin[0], magbiasMin[1], magbiasMin[2]); pc.serial.printf("Magbias (Max) : %f, %f, %f\r\n", magbiasMax[0], magbiasMax[1], magbiasMax[2]); magCalibrator.getExtremes(magbiasMin,magbiasMax); pc.serial.printf("Calculating pitch/roll Offset \r\n"); //姿勢オフセットを計算 rpy_align.y = 0.0f*M_PI/180.0f; rpy_align.x = 0.0f*M_PI/180.0f; float ave_pitch = 0.0f; float ave_roll = 0.0f; Timer _t; _t.start(); for (int i = 0 ; i < 2200; i++) { float tstart = _t.read(); //姿勢角を更新 getIMUval(); //ekf.updateBetweenMeasures(gyro, att_dt); //ekf.updateAcrossMeasures(LPmag/LPmag.Norm(), magref/magref.Norm(), ekf.Rmag); //ekf.updateAcrossMeasures(LPacc/LPacc.Norm(), accref/accref.Norm(), ekf.Racc); //ekf.computeAngles(rpy, rpy_g, rpy_align); if(i>199) { ave_pitch += rpy.y; ave_roll += rpy.x; } wait(0.001); float tend = _t.read(); att_dt = (tend-tstart); } pc.serial.printf("aliginment data : %f(pitch deg) %f(roll deg)\r\n",ave_pitch/2000.0f*180.0f/M_PI,ave_roll/2000.0f*180.0f/M_PI); while(1) { wait(1000); } }