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Fork of Quadrocopter by
main.cpp
- Committer:
- MarcoF89
- Date:
- 2017-09-11
- Revision:
- 19:ac98ad146067
- Parent:
- 18:78e7de067ddb
- Child:
- 20:76e25a3c8684
File content as of revision 19:ac98ad146067:
#include <Timer.h> #include <math.h> #include "mbed.h" #include "stdio.h" #include "deklaration.h" #include "messen.h" #include "filter/Kalman.h" #define RAD 57.29577951 uint16_t zeit; uint32_t zeit2; uint8_t k; int main() { gain_g = 0; z_off = 0; zeit = 0; k = 0; drift_z = 0; Motor1.period_ms(2); Motor2.period_ms(2); Motor3.period_ms(2); Motor4.period_ms(2); initialisierung_gyro(); initialisierung_acc(); Kalman(&Q_angle, &Q_bias, &R_measure, &bias, P); if (taster2) { viberationen(&rauschen, &Motor1, &Motor2, &Motor3, &Motor4, &taster4); } if (taster3) { anlernen(&Motor1, &Motor2, &Motor3, &Motor4, &taster1, &taster2, &taster4); } pc.printf("Druecke Taster1 fuer den Start\n\r"); n1=n2=n3=n4=700; if (taster1) { uint16_t flanke1,hilfe1=0,flanke2,hilfe2=0,flanke3,hilfe3=0,flanke4,hilfe4=0; pc.printf("Taster-Modus aktiv\n\r"); n1=n2=n3=n4=625; while(1) { flanke2 = taster2; if ((flanke2 != 0) && (hilfe2 == 0)) { n1+=50; n2+=50; n3+=50; n4+=50; } hilfe2=flanke2; flanke3 = taster3; if ((flanke3 != 0) && (hilfe3 == 0)) { n1-=50; n2-=50; n3-=50; n4-=50; } hilfe3=flanke3; flanke4 = taster4; if ((flanke4 != 0) && (hilfe4 == 0)) { n1=n2=n3=n4=625; } hilfe4=flanke4; Motor1.pulsewidth_us(n1); Motor2.pulsewidth_us(n2); Motor3.pulsewidth_us(n3); Motor4.pulsewidth_us(n4); pc.printf("Drehzahl= %d\r= %d",n1); } } while(1) { if (taster1) { while(1)//(!taster4) { pc.printf("\n\rOffset und Driftberechnung wird durchgefuehrt, halte die Drohne still"); offset_gyro(&z_off, &x_off, &y_off); drift_gyro(&drift_z, &drift_x, &drift_y, &timer, &timer2, &gain_g, &roll_g, &pitch_g, &z_off, &x_off, &y_off); pc.printf("\n\rOffgesamt:\n\rZ = %3.5f\tY = %3.5f\tZ = %3.5f\t\n\r", z_off, x_off, y_off); pc.printf("\n\rDrift:Z: %3.10f\tX: %3.10f\tY: %3.10f\n\r", drift_z, drift_x, drift_y); /********//******/ /*Messen*//*Gyro*/ /********//******/ timer.stop(); timer2.stop(); timer.reset(); timer2.reset(); gain_g = 0; pitch_g = 0; roll_g = 0; timer.start(); timer2.start(); int i = 0; while(1) { i++; zeit = timer.read_us(); timer.reset(); aktuell_roh(&z_g, &x_g, &y_g, &z_a, &x_a, &y_a); gain_g = gain_g + ((z_g - z_off) * 1/16.4); pitch_g = pitch_g + ((y_g - y_off) * 1/16.4); roll_g = roll_g + ((x_g - x_off) * 1/16.4); y = y_a / 16384.00; x = x_a / 16384.00; z = z_a / 16384.00; roll_a = atan2(y, sqrt(x * x + z * z)) * RAD; pitch_a = atan2(-x, z) * RAD; if (timer2.read_ms() >= 2000) { gain_g -= drift_z; pitch_g -= drift_y; roll_g -= drift_x; timer2.reset(); } gain = gain_g; pitch = pitch_g * 0.9 + pitch_a * 0.1; roll = roll_g * 0.9 + roll_a * 0.1; if (i == 2000) { pc.printf("gain: %2.5f\tpitch: %2.5f\troll: %2.5f\t\n\r",pitch, roll, gain); i = 0; } } } } } }