Einstein Filho
/
MANGUEBAJA2019_FRONT2
Mangue Baja team's code to frontal ECU
Kalman/Kalman.cpp@0:12fb9cbcabcc, 2019-07-24 (annotated)
- Committer:
- einsteingustavo
- Date:
- Wed Jul 24 20:03:52 2019 +0000
- Revision:
- 0:12fb9cbcabcc
Mangue Baja team's code to frontal ECU
Who changed what in which revision?
User | Revision | Line number | New contents of line |
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einsteingustavo | 0:12fb9cbcabcc | 1 | /* Copyright (C) 2012 Kristian Lauszus, TKJ Electronics. All rights reserved. |
einsteingustavo | 0:12fb9cbcabcc | 2 | |
einsteingustavo | 0:12fb9cbcabcc | 3 | This software may be distributed and modified under the terms of the GNU |
einsteingustavo | 0:12fb9cbcabcc | 4 | General Public License version 2 (GPL2) as published by the Free Software |
einsteingustavo | 0:12fb9cbcabcc | 5 | Foundation and appearing in the file GPL2.TXT included in the packaging of |
einsteingustavo | 0:12fb9cbcabcc | 6 | this file. Please note that GPL2 Section 2[b] requires that all works based |
einsteingustavo | 0:12fb9cbcabcc | 7 | on this software must also be made publicly available under the terms of |
einsteingustavo | 0:12fb9cbcabcc | 8 | the GPL2 ("Copyleft"). |
einsteingustavo | 0:12fb9cbcabcc | 9 | |
einsteingustavo | 0:12fb9cbcabcc | 10 | Contact information |
einsteingustavo | 0:12fb9cbcabcc | 11 | ------------------- |
einsteingustavo | 0:12fb9cbcabcc | 12 | |
einsteingustavo | 0:12fb9cbcabcc | 13 | Kristian Lauszus, TKJ Electronics |
einsteingustavo | 0:12fb9cbcabcc | 14 | Web : http://www.tkjelectronics.com |
einsteingustavo | 0:12fb9cbcabcc | 15 | e-mail : kristianl@tkjelectronics.com |
einsteingustavo | 0:12fb9cbcabcc | 16 | */ |
einsteingustavo | 0:12fb9cbcabcc | 17 | |
einsteingustavo | 0:12fb9cbcabcc | 18 | #include "Kalman.h" |
einsteingustavo | 0:12fb9cbcabcc | 19 | |
einsteingustavo | 0:12fb9cbcabcc | 20 | Kalman::Kalman() { |
einsteingustavo | 0:12fb9cbcabcc | 21 | /* We will set the variables like so, these can also be tuned by the user */ |
einsteingustavo | 0:12fb9cbcabcc | 22 | Q_angle = 0.001f; |
einsteingustavo | 0:12fb9cbcabcc | 23 | Q_bias = 0.003f; |
einsteingustavo | 0:12fb9cbcabcc | 24 | R_measure = 0.03f; |
einsteingustavo | 0:12fb9cbcabcc | 25 | |
einsteingustavo | 0:12fb9cbcabcc | 26 | angle = 0.0f; // Reset the angle |
einsteingustavo | 0:12fb9cbcabcc | 27 | bias = 0.0f; // Reset bias |
einsteingustavo | 0:12fb9cbcabcc | 28 | |
einsteingustavo | 0:12fb9cbcabcc | 29 | P[0][0] = 0.0f; // Since we assume that the bias is 0 and we know the starting angle (use setAngle), the error covariance matrix is set like so - see: http://en.wikipedia.org/wiki/Kalman_filter#Example_application.2C_technical |
einsteingustavo | 0:12fb9cbcabcc | 30 | P[0][1] = 0.0f; |
einsteingustavo | 0:12fb9cbcabcc | 31 | P[1][0] = 0.0f; |
einsteingustavo | 0:12fb9cbcabcc | 32 | P[1][1] = 0.0f; |
einsteingustavo | 0:12fb9cbcabcc | 33 | }; |
einsteingustavo | 0:12fb9cbcabcc | 34 | |
einsteingustavo | 0:12fb9cbcabcc | 35 | // The angle should be in degrees and the rate should be in degrees per second and the delta time in seconds |
einsteingustavo | 0:12fb9cbcabcc | 36 | float Kalman::getAngle(float newAngle, float newRate, float dt) { |
einsteingustavo | 0:12fb9cbcabcc | 37 | // KasBot V2 - Kalman filter module - http://www.x-firm.com/?page_id=145 |
einsteingustavo | 0:12fb9cbcabcc | 38 | // Modified by Kristian Lauszus |
einsteingustavo | 0:12fb9cbcabcc | 39 | // See my blog post for more information: http://blog.tkjelectronics.dk/2012/09/a-practical-approach-to-kalman-filter-and-how-to-implement-it |
einsteingustavo | 0:12fb9cbcabcc | 40 | |
einsteingustavo | 0:12fb9cbcabcc | 41 | // Discrete Kalman filter time update equations - Time Update ("Predict") |
einsteingustavo | 0:12fb9cbcabcc | 42 | // Update xhat - Project the state ahead |
einsteingustavo | 0:12fb9cbcabcc | 43 | /* Step 1 */ |
einsteingustavo | 0:12fb9cbcabcc | 44 | rate = newRate - bias; |
einsteingustavo | 0:12fb9cbcabcc | 45 | angle += dt * rate; |
einsteingustavo | 0:12fb9cbcabcc | 46 | |
einsteingustavo | 0:12fb9cbcabcc | 47 | // Update estimation error covariance - Project the error covariance ahead |
einsteingustavo | 0:12fb9cbcabcc | 48 | /* Step 2 */ |
einsteingustavo | 0:12fb9cbcabcc | 49 | P[0][0] += dt * (dt*P[1][1] - P[0][1] - P[1][0] + Q_angle); |
einsteingustavo | 0:12fb9cbcabcc | 50 | P[0][1] -= dt * P[1][1]; |
einsteingustavo | 0:12fb9cbcabcc | 51 | P[1][0] -= dt * P[1][1]; |
einsteingustavo | 0:12fb9cbcabcc | 52 | P[1][1] += Q_bias * dt; |
einsteingustavo | 0:12fb9cbcabcc | 53 | |
einsteingustavo | 0:12fb9cbcabcc | 54 | // Discrete Kalman filter measurement update equations - Measurement Update ("Correct") |
einsteingustavo | 0:12fb9cbcabcc | 55 | // Calculate Kalman gain - Compute the Kalman gain |
einsteingustavo | 0:12fb9cbcabcc | 56 | /* Step 4 */ |
einsteingustavo | 0:12fb9cbcabcc | 57 | float S = P[0][0] + R_measure; // Estimate error |
einsteingustavo | 0:12fb9cbcabcc | 58 | /* Step 5 */ |
einsteingustavo | 0:12fb9cbcabcc | 59 | float K[2]; // Kalman gain - This is a 2x1 vector |
einsteingustavo | 0:12fb9cbcabcc | 60 | K[0] = P[0][0] / S; |
einsteingustavo | 0:12fb9cbcabcc | 61 | K[1] = P[1][0] / S; |
einsteingustavo | 0:12fb9cbcabcc | 62 | |
einsteingustavo | 0:12fb9cbcabcc | 63 | // Calculate angle and bias - Update estimate with measurement zk (newAngle) |
einsteingustavo | 0:12fb9cbcabcc | 64 | /* Step 3 */ |
einsteingustavo | 0:12fb9cbcabcc | 65 | float y = newAngle - angle; // Angle difference |
einsteingustavo | 0:12fb9cbcabcc | 66 | /* Step 6 */ |
einsteingustavo | 0:12fb9cbcabcc | 67 | angle += K[0] * y; |
einsteingustavo | 0:12fb9cbcabcc | 68 | bias += K[1] * y; |
einsteingustavo | 0:12fb9cbcabcc | 69 | |
einsteingustavo | 0:12fb9cbcabcc | 70 | // Calculate estimation error covariance - Update the error covariance |
einsteingustavo | 0:12fb9cbcabcc | 71 | /* Step 7 */ |
einsteingustavo | 0:12fb9cbcabcc | 72 | float P00_temp = P[0][0]; |
einsteingustavo | 0:12fb9cbcabcc | 73 | float P01_temp = P[0][1]; |
einsteingustavo | 0:12fb9cbcabcc | 74 | |
einsteingustavo | 0:12fb9cbcabcc | 75 | P[0][0] -= K[0] * P00_temp; |
einsteingustavo | 0:12fb9cbcabcc | 76 | P[0][1] -= K[0] * P01_temp; |
einsteingustavo | 0:12fb9cbcabcc | 77 | P[1][0] -= K[1] * P00_temp; |
einsteingustavo | 0:12fb9cbcabcc | 78 | P[1][1] -= K[1] * P01_temp; |
einsteingustavo | 0:12fb9cbcabcc | 79 | |
einsteingustavo | 0:12fb9cbcabcc | 80 | return angle; |
einsteingustavo | 0:12fb9cbcabcc | 81 | } |
einsteingustavo | 0:12fb9cbcabcc | 82 | |
einsteingustavo | 0:12fb9cbcabcc | 83 | void Kalman::setAngle(float angle) { this->angle = angle; }; // Used to set angle, this should be set as the starting angle |
einsteingustavo | 0:12fb9cbcabcc | 84 | float Kalman::getRate() { return this->rate; }; // Return the unbiased rate |
einsteingustavo | 0:12fb9cbcabcc | 85 | |
einsteingustavo | 0:12fb9cbcabcc | 86 | /* These are used to tune the Kalman filter */ |
einsteingustavo | 0:12fb9cbcabcc | 87 | void Kalman::setQangle(float Q_angle) { this->Q_angle = Q_angle; }; |
einsteingustavo | 0:12fb9cbcabcc | 88 | void Kalman::setQbias(float Q_bias) { this->Q_bias = Q_bias; }; |
einsteingustavo | 0:12fb9cbcabcc | 89 | void Kalman::setRmeasure(float R_measure) { this->R_measure = R_measure; }; |
einsteingustavo | 0:12fb9cbcabcc | 90 | |
einsteingustavo | 0:12fb9cbcabcc | 91 | float Kalman::getQangle() { return this->Q_angle; }; |
einsteingustavo | 0:12fb9cbcabcc | 92 | float Kalman::getQbias() { return this->Q_bias; }; |
einsteingustavo | 0:12fb9cbcabcc | 93 | float Kalman::getRmeasure() { return this->R_measure; }; |
einsteingustavo | 0:12fb9cbcabcc | 94 |