David Lakata / Mbed 2 deprecated QuadTrio

ESE350 project, Spring 2016, University of Pennsylvania

Dependencies:   Adafruit9-DOf Receiver mbed-rtos mbed

main.cpp@6:6f3ffd97d808, 2016-04-02 (annotated)

Committer:
ivo_david_michelle
Date:
Sat Apr 02 13:13:41 2016 +0000
Revision:
6:6f3ffd97d808
Parent:
5:f007542f1dab
Child:
7:f3f94eadc5b5
started implementing quadcopter class;

Who changed what in which revision?

UserRevisionLine numberNew contents of line
ivo_david_michelle 0:4c04e4fd1310 1 #include "mbed.h"
ivo_david_michelle 1:b87e95907a18 2 #define _MBED_
ivo_david_michelle 1:b87e95907a18 3 #include "Adafruit_9DOF.h"
ivo_david_michelle 1:b87e95907a18 4 #include "Serial_base.h"
ivo_david_michelle 1:b87e95907a18 5 #include "controller.h"
ivo_david_michelle 3:828e82089564 6 #include "sensor.h"
ivo_david_michelle 1:b87e95907a18 7
ivo_david_michelle 1:b87e95907a18 8 DigitalOut myled(LED1);
ivo_david_michelle 1:b87e95907a18 9 Adafruit_9DOF dof = Adafruit_9DOF();
ivo_david_michelle 1:b87e95907a18 10 Adafruit_LSM303_Accel_Unified accel = Adafruit_LSM303_Accel_Unified(30301);
ivo_david_michelle 1:b87e95907a18 11 Adafruit_LSM303_Mag_Unified mag = Adafruit_LSM303_Mag_Unified(30302);
ivo_david_michelle 1:b87e95907a18 12 Adafruit_L3GD20_Unified gyro = Adafruit_L3GD20_Unified(20);
ivo_david_michelle 0:4c04e4fd1310 13
ivo_david_michelle 0:4c04e4fd1310 14 Serial pc(USBTX, USBRX);
ivo_david_michelle 0:4c04e4fd1310 15
ivo_david_michelle 6:6f3ffd97d808 16 // pwm outputs for the 4 motors (motor 1 points into x direction, 2 into y direction, 3 -x direction, -y direction
ivo_david_michelle 4:3040d0f9e8c6 17 PwmOut motor_1(p21);
ivo_david_michelle 5:f007542f1dab 18 PwmOut motor_2(p22);
ivo_david_michelle 4:3040d0f9e8c6 19 PwmOut motor_3(p23);
ivo_david_michelle 4:3040d0f9e8c6 20 PwmOut motor_4(p24);
ivo_david_michelle 4:3040d0f9e8c6 21
ivo_david_michelle 0:4c04e4fd1310 22 int main()
ivo_david_michelle 0:4c04e4fd1310 23 {
ivo_david_michelle 6:6f3ffd97d808 24 control result;
ivo_david_michelle 4:3040d0f9e8c6 25 offset offset_gyro;
ivo_david_michelle 3:828e82089564 26
ivo_david_michelle 3:828e82089564 27 initSensors(accel, mag, gyro,offset_gyro);
ivo_david_michelle 1:b87e95907a18 28
ivo_david_michelle 1:b87e95907a18 29 sensors_event_t accel_event;
ivo_david_michelle 1:b87e95907a18 30 sensors_event_t mag_event;
ivo_david_michelle 1:b87e95907a18 31 sensors_event_t gyro_event;
ivo_david_michelle 1:b87e95907a18 32 sensors_vec_t orientation;
ivo_david_michelle 4:3040d0f9e8c6 33
ivo_david_michelle 6:6f3ffd97d808 34 motor_1.period(0.002); // motor requires a 2ms period
ivo_david_michelle 6:6f3ffd97d808 35 motor_2.period(0.002); // motor requires a 2ms period
ivo_david_michelle 6:6f3ffd97d808 36 motor_3.period(0.002); // motor requires a 2ms period
ivo_david_michelle 6:6f3ffd97d808 37 motor_4.period(0.002); // motor requires a 2ms period
ivo_david_michelle 4:3040d0f9e8c6 38
ivo_david_michelle 4:3040d0f9e8c6 39 // pwm duty cycles for the 4 motors
ivo_david_michelle 4:3040d0f9e8c6 40 motor_1 = 0;
ivo_david_michelle 4:3040d0f9e8c6 41 motor_2 = 0;
ivo_david_michelle 4:3040d0f9e8c6 42 motor_3 = 0;
ivo_david_michelle 4:3040d0f9e8c6 43 motor_4 = 0;
ivo_david_michelle 4:3040d0f9e8c6 44
ivo_david_michelle 4:3040d0f9e8c6 45 // startup procedure
ivo_david_michelle 4:3040d0f9e8c6 46 pc.printf("Type 's' to start up Motors, or anything else to abort.\n\r");
ivo_david_michelle 4:3040d0f9e8c6 47 char a= pc.getc();
ivo_david_michelle 4:3040d0f9e8c6 48 if (a!='s') {
ivo_david_michelle 4:3040d0f9e8c6 49 pc.printf("Aborting");
ivo_david_michelle 4:3040d0f9e8c6 50 return 0;
ivo_david_michelle 4:3040d0f9e8c6 51 };
ivo_david_michelle 4:3040d0f9e8c6 52 pc.printf("Starting up ESCs\n\r");
ivo_david_michelle 4:3040d0f9e8c6 53 motor_1 = 0.5;
ivo_david_michelle 4:3040d0f9e8c6 54 motor_2 = 0.5;
ivo_david_michelle 4:3040d0f9e8c6 55 motor_3 = 0.5;
ivo_david_michelle 4:3040d0f9e8c6 56 motor_4 = 0.5;
ivo_david_michelle 4:3040d0f9e8c6 57
ivo_david_michelle 4:3040d0f9e8c6 58 pc.printf("Type 'c' to enter control loop, or anything else to abort.\n\r");
ivo_david_michelle 4:3040d0f9e8c6 59 char b= pc.getc();
ivo_david_michelle 4:3040d0f9e8c6 60 if (b!='c') {
ivo_david_michelle 4:3040d0f9e8c6 61 pc.printf("Aborting");
ivo_david_michelle 4:3040d0f9e8c6 62 return 0;
ivo_david_michelle 4:3040d0f9e8c6 63 };
ivo_david_michelle 4:3040d0f9e8c6 64
ivo_david_michelle 4:3040d0f9e8c6 65 pc.printf("Entering control loop\n\r");
ivo_david_michelle 4:3040d0f9e8c6 66
ivo_david_michelle 4:3040d0f9e8c6 67 while (1) {
ivo_david_michelle 1:b87e95907a18 68 /* Calculate pitch and roll from the raw accelerometer data */
ivo_david_michelle 1:b87e95907a18 69 accel.getEvent(&accel_event);
ivo_david_michelle 1:b87e95907a18 70 if (dof.accelGetOrientation(&accel_event, &orientation)) {
ivo_david_michelle 1:b87e95907a18 71 /* 'orientation' should have valid .roll and .pitch fields */
ivo_david_michelle 1:b87e95907a18 72 //s_com->print(("Roll: "));
ivo_david_michelle 1:b87e95907a18 73 //s_com->print(orientation.roll);
ivo_david_michelle 1:b87e95907a18 74 //s_com->print(("; "));
ivo_david_michelle 1:b87e95907a18 75 //s_com->print(("Pitch: "));
ivo_david_michelle 1:b87e95907a18 76 //s_com->print(orientation.pitch);
ivo_david_michelle 1:b87e95907a18 77 //s_com->print((";\t"));
ivo_david_michelle 1:b87e95907a18 78 }
ivo_david_michelle 1:b87e95907a18 79 /* Calculate the heading using the magnetometer */
ivo_david_michelle 1:b87e95907a18 80 mag.getEvent(&mag_event);
ivo_david_michelle 1:b87e95907a18 81 if (dof.magGetOrientation(SENSOR_AXIS_Z, &mag_event, &orientation)) {
ivo_david_michelle 1:b87e95907a18 82 /* 'orientation' should have valid .heading data now */
ivo_david_michelle 1:b87e95907a18 83 //s_com->print(("Heading: "));
ivo_david_michelle 1:b87e95907a18 84 //s_com->print(orientation.heading);
ivo_david_michelle 4:3040d0f9e8c6 85 // s_com->print((";\r\n"));
ivo_david_michelle 1:b87e95907a18 86 }
ivo_david_michelle 1:b87e95907a18 87 /* Get angular rate data from gyroscope */
ivo_david_michelle 1:b87e95907a18 88 gyro.getEvent(&gyro_event);
ivo_david_michelle 3:828e82089564 89 gyro_event.gyro.x -= offset_gyro.x_offset;
ivo_david_michelle 3:828e82089564 90 gyro_event.gyro.y -= offset_gyro.y_offset;
ivo_david_michelle 3:828e82089564 91 gyro_event.gyro.z -= offset_gyro.z_offset;
ivo_david_michelle 1:b87e95907a18 92
ivo_david_michelle 5:f007542f1dab 93 wait(0.01);
ivo_david_michelle 1:b87e95907a18 94
ivo_david_michelle 0:4c04e4fd1310 95 // get sensor values
ivo_david_michelle 0:4c04e4fd1310 96
ivo_david_michelle 0:4c04e4fd1310 97 // call controller
ivo_david_michelle 2:c041e434eab6 98 controller(gyro_event, orientation, &result);
ivo_david_michelle 0:4c04e4fd1310 99
ivo_david_michelle 4:3040d0f9e8c6 100 // compute PWM singals
ivo_david_michelle 4:3040d0f9e8c6 101 // assumption for low angles the computed moments are between -10...10
ivo_david_michelle 4:3040d0f9e8c6 102 // since I dont want to risk, i set PWM to 60% duty cycle if deflection =10.
ivo_david_michelle 4:3040d0f9e8c6 103 // USB connection of quadcopter points into x direction.
ivo_david_michelle 4:3040d0f9e8c6 104
ivo_david_michelle 4:3040d0f9e8c6 105
ivo_david_michelle 4:3040d0f9e8c6 106 // Set duty cycle
ivo_david_michelle 4:3040d0f9e8c6 107 // continue looking what pwm is.
ivo_david_michelle 5:f007542f1dab 108
ivo_david_michelle 5:f007542f1dab 109 motor_2=0.6+result.M_x/100;
ivo_david_michelle 5:f007542f1dab 110 motor_4=0.6-result.M_x/100;
ivo_david_michelle 4:3040d0f9e8c6 111
ivo_david_michelle 4:3040d0f9e8c6 112
ivo_david_michelle 0:4c04e4fd1310 113 // plot
ivo_david_michelle 0:4c04e4fd1310 114
ivo_david_michelle 0:4c04e4fd1310 115 //pc.printf("F: %f M_x: %f M_y: %f M_z: %f\n\r", F, M_x, M_y, M_z);
ivo_david_michelle 2:c041e434eab6 116 pc.printf("M_x: %f\tM_y: %f\tM_z: %f\tF: %f\n\r", result.M_x, result.M_y, result.M_z, result.F);
ivo_david_michelle 0:4c04e4fd1310 117 }
ivo_david_michelle 0:4c04e4fd1310 118 }