xyControl  0.1
Quadrotor Flight Controller on AVR Basis
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pid.c
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1 /*
2  * pid.c
3  *
4  * Copyright (c) 2013, Thomas Buck <xythobuz@me.com>
5  * All rights reserved.
6  *
7  * Redistribution and use in source and binary forms, with or without
8  * modification, are permitted provided that the following conditions
9  * are met:
10  *
11  * - Redistributions of source code must retain the above copyright notice,
12  * this list of conditions and the following disclaimer.
13  *
14  * - Redistributions in binary form must reproduce the above copyright
15  * notice, this list of conditions and the following disclaimer in the
16  * documentation and/or other materials provided with the distribution.
17  *
18  * THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS
19  * "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT LIMITED
20  * TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS FOR A PARTICULAR
21  * PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE COPYRIGHT HOLDER OR
22  * CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT, INCIDENTAL, SPECIAL,
23  * EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING, BUT NOT LIMITED TO,
24  * PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS OF USE, DATA, OR
25  * PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED AND ON ANY THEORY OF
26  * LIABILITY, WHETHER IN CONTRACT, STRICT LIABILITY, OR TORT (INCLUDING
27  * NEGLIGENCE OR OTHERWISE) ARISING IN ANY WAY OUT OF THE USE OF THIS
28  * SOFTWARE, EVEN IF ADVISED OF THE POSSIBILITY OF SUCH DAMAGE.
29  */
30 #include <stdint.h>
31 #include <avr/io.h>
32 
33 #include <twi.h>
34 #include <motor.h>
35 #include <tasks.h>
36 #include <time.h>
37 #include <pid.h>
38 #include <orientation.h>
39 #include <config.h>
40 
51 double pidTarget[2];
52 double pidOutput[2];
53 
54 double pidExecute(double should, double is, PIDState *state) {
55  time_t now = getSystemTime();
56  double timeChange = (double)(now - state->last);
57  double error = should - is;
58  double newErrorSum = state->sumError + (error * timeChange);
59  if ((newErrorSum >= state->intMin) && (newErrorSum <= state->intMax))
60  state->sumError = newErrorSum; // Prevent Integral Windup
61  double dError = (error - state->lastError) / timeChange;
62  double output = (state->kp * error) + (state->ki * state->sumError) + (state->kd * dError);
63  state->lastError = error;
64  state->last = now;
65  if (output > state->outMax) {
66  output = state->outMax;
67  }
68  if (output < state->outMin) {
69  output = state->outMin;
70  }
71  return output;
72 }
73 
74 void pidInit(void) {
75  for (uint8_t i = 0; i < 2; i++) {
77  pidTarget[i] = 0.0;
78  }
79 }
80 
81 void pidSet(PIDState *pid, double kp, double ki, double kd, double min, double max, double iMin, double iMax) {
82  pid->kp = kp;
83  pid->ki = ki;
84  pid->kd = kd;
85  pid->outMin = min;
86  pid->outMax = max;
87  pid->intMin = iMin;
88  pid->intMax = iMax;
89  pid->lastError = 0;
90  pid->sumError = 0;
91  pid->last = 0;
92 }
93 
94 void pidTask(void) {
95  pidOutput[ROLL] = pidExecute(pidTarget[ROLL], orientation.roll, &pidStates[ROLL]);
96  pidOutput[PITCH] = pidExecute(pidTarget[PITCH], orientation.pitch, &pidStates[PITCH]);
97 }