Latest version of my quadcopter controller with an LPC1768 and MPU9250.
Currently running on a custom PCB with 30.5 x 30.5mm mounts. There are also 2 PC apps that go with the software; one to set up the PID controller and one to balance the motors and props. If anyone is interested, send me a message and I'll upload them.
Madgwick/MadgwickAHRS.cpp@5:0f4204941604, 2018-07-13 (annotated)
- Committer:
- Anaesthetix
- Date:
- Fri Jul 13 14:27:30 2018 +0000
- Revision:
- 5:0f4204941604
- Parent:
- 0:0929d3d566cf
Yaw PID added
Who changed what in which revision?
User | Revision | Line number | New contents of line |
---|---|---|---|
Anaesthetix | 0:0929d3d566cf | 1 | //============================================================================================= |
Anaesthetix | 0:0929d3d566cf | 2 | // MadgwickAHRS.c |
Anaesthetix | 0:0929d3d566cf | 3 | //============================================================================================= |
Anaesthetix | 0:0929d3d566cf | 4 | // |
Anaesthetix | 0:0929d3d566cf | 5 | // Implementation of Madgwick's IMU and AHRS algorithms. |
Anaesthetix | 0:0929d3d566cf | 6 | // See: http://www.x-io.co.uk/open-source-imu-and-ahrs-algorithms/ |
Anaesthetix | 0:0929d3d566cf | 7 | // |
Anaesthetix | 0:0929d3d566cf | 8 | // From the x-io website "Open-source resources available on this website are |
Anaesthetix | 0:0929d3d566cf | 9 | // provided under the GNU General Public Licence unless an alternative licence |
Anaesthetix | 0:0929d3d566cf | 10 | // is provided in source." |
Anaesthetix | 0:0929d3d566cf | 11 | // |
Anaesthetix | 0:0929d3d566cf | 12 | // Date Author Notes |
Anaesthetix | 0:0929d3d566cf | 13 | // 29/09/2011 SOH Madgwick Initial release |
Anaesthetix | 0:0929d3d566cf | 14 | // 02/10/2011 SOH Madgwick Optimised for reduced CPU load |
Anaesthetix | 0:0929d3d566cf | 15 | // 19/02/2012 SOH Madgwick Magnetometer measurement is normalised |
Anaesthetix | 0:0929d3d566cf | 16 | // |
Anaesthetix | 0:0929d3d566cf | 17 | //============================================================================================= |
Anaesthetix | 0:0929d3d566cf | 18 | |
Anaesthetix | 0:0929d3d566cf | 19 | //------------------------------------------------------------------------------------------- |
Anaesthetix | 0:0929d3d566cf | 20 | // Header files |
Anaesthetix | 0:0929d3d566cf | 21 | |
Anaesthetix | 0:0929d3d566cf | 22 | #include "MadgwickAHRS.h" |
Anaesthetix | 0:0929d3d566cf | 23 | #include <math.h> |
Anaesthetix | 0:0929d3d566cf | 24 | |
Anaesthetix | 0:0929d3d566cf | 25 | //------------------------------------------------------------------------------------------- |
Anaesthetix | 0:0929d3d566cf | 26 | // Definitions |
Anaesthetix | 0:0929d3d566cf | 27 | |
Anaesthetix | 0:0929d3d566cf | 28 | #define sampleFreqDef 1500.0f // sample frequency in Hz |
Anaesthetix | 0:0929d3d566cf | 29 | #define betaDef 0.1f // 2 * proportional gain 0.1 - 0.5 - 5 was 2.5 |
Anaesthetix | 0:0929d3d566cf | 30 | |
Anaesthetix | 0:0929d3d566cf | 31 | |
Anaesthetix | 0:0929d3d566cf | 32 | //============================================================================================ |
Anaesthetix | 0:0929d3d566cf | 33 | // Functions |
Anaesthetix | 0:0929d3d566cf | 34 | |
Anaesthetix | 0:0929d3d566cf | 35 | //------------------------------------------------------------------------------------------- |
Anaesthetix | 0:0929d3d566cf | 36 | // AHRS algorithm update |
Anaesthetix | 0:0929d3d566cf | 37 | |
Anaesthetix | 5:0f4204941604 | 38 | Madgwick::Madgwick() |
Anaesthetix | 5:0f4204941604 | 39 | { |
Anaesthetix | 0:0929d3d566cf | 40 | beta = betaDef; |
Anaesthetix | 0:0929d3d566cf | 41 | q0 = 1.0f; |
Anaesthetix | 0:0929d3d566cf | 42 | q1 = 0.0f; |
Anaesthetix | 0:0929d3d566cf | 43 | q2 = 0.0f; |
Anaesthetix | 0:0929d3d566cf | 44 | q3 = 0.0f; |
Anaesthetix | 0:0929d3d566cf | 45 | invSampleFreq = 1.0f / sampleFreqDef; |
Anaesthetix | 0:0929d3d566cf | 46 | anglesComputed = 0; |
Anaesthetix | 0:0929d3d566cf | 47 | } |
Anaesthetix | 0:0929d3d566cf | 48 | |
Anaesthetix | 5:0f4204941604 | 49 | void Madgwick::update(float gx, float gy, float gz, float ax, float ay, float az, float mx, float my, float mz) |
Anaesthetix | 5:0f4204941604 | 50 | { |
Anaesthetix | 0:0929d3d566cf | 51 | float recipNorm; |
Anaesthetix | 0:0929d3d566cf | 52 | float s0, s1, s2, s3; |
Anaesthetix | 0:0929d3d566cf | 53 | float qDot1, qDot2, qDot3, qDot4; |
Anaesthetix | 0:0929d3d566cf | 54 | float hx, hy; |
Anaesthetix | 0:0929d3d566cf | 55 | float _2q0mx, _2q0my, _2q0mz, _2q1mx, _2bx, _2bz, _4bx, _4bz, _8bx, _8bz, _2q0, _2q1, _2q2, _2q3, _2q0q2, _2q2q3, q0q0, q0q1, q0q2, q0q3, q1q1, q1q2, q1q3, q2q2, q2q3, q3q3; |
Anaesthetix | 0:0929d3d566cf | 56 | |
Anaesthetix | 0:0929d3d566cf | 57 | // Use IMU algorithm if magnetometer measurement invalid (avoids NaN in magnetometer normalisation) |
Anaesthetix | 0:0929d3d566cf | 58 | if((mx == 0.0f) && (my == 0.0f) && (mz == 0.0f)) { |
Anaesthetix | 0:0929d3d566cf | 59 | updateIMU(gx, gy, gz, ax, ay, az); |
Anaesthetix | 0:0929d3d566cf | 60 | return; |
Anaesthetix | 0:0929d3d566cf | 61 | } |
Anaesthetix | 0:0929d3d566cf | 62 | |
Anaesthetix | 0:0929d3d566cf | 63 | // Convert gyroscope degrees/sec to radians/sec |
Anaesthetix | 0:0929d3d566cf | 64 | gx *= 0.0174533f; |
Anaesthetix | 0:0929d3d566cf | 65 | gy *= 0.0174533f; |
Anaesthetix | 0:0929d3d566cf | 66 | gz *= 0.0174533f; |
Anaesthetix | 0:0929d3d566cf | 67 | |
Anaesthetix | 0:0929d3d566cf | 68 | // Rate of change of quaternion from gyroscope |
Anaesthetix | 0:0929d3d566cf | 69 | qDot1 = 0.5f * (-q1 * gx - q2 * gy - q3 * gz); |
Anaesthetix | 0:0929d3d566cf | 70 | qDot2 = 0.5f * (q0 * gx + q2 * gz - q3 * gy); |
Anaesthetix | 0:0929d3d566cf | 71 | qDot3 = 0.5f * (q0 * gy - q1 * gz + q3 * gx); |
Anaesthetix | 0:0929d3d566cf | 72 | qDot4 = 0.5f * (q0 * gz + q1 * gy - q2 * gx); |
Anaesthetix | 0:0929d3d566cf | 73 | |
Anaesthetix | 0:0929d3d566cf | 74 | // Compute feedback only if accelerometer measurement valid (avoids NaN in accelerometer normalisation) |
Anaesthetix | 0:0929d3d566cf | 75 | if(!((ax == 0.0f) && (ay == 0.0f) && (az == 0.0f))) { |
Anaesthetix | 0:0929d3d566cf | 76 | |
Anaesthetix | 0:0929d3d566cf | 77 | // Normalise accelerometer measurement |
Anaesthetix | 0:0929d3d566cf | 78 | recipNorm = invSqrt(ax * ax + ay * ay + az * az); |
Anaesthetix | 0:0929d3d566cf | 79 | ax *= recipNorm; |
Anaesthetix | 0:0929d3d566cf | 80 | ay *= recipNorm; |
Anaesthetix | 0:0929d3d566cf | 81 | az *= recipNorm; |
Anaesthetix | 0:0929d3d566cf | 82 | |
Anaesthetix | 0:0929d3d566cf | 83 | // Normalise magnetometer measurement |
Anaesthetix | 0:0929d3d566cf | 84 | recipNorm = invSqrt(mx * mx + my * my + mz * mz); |
Anaesthetix | 0:0929d3d566cf | 85 | mx *= recipNorm; |
Anaesthetix | 0:0929d3d566cf | 86 | my *= recipNorm; |
Anaesthetix | 0:0929d3d566cf | 87 | mz *= recipNorm; |
Anaesthetix | 0:0929d3d566cf | 88 | |
Anaesthetix | 0:0929d3d566cf | 89 | // Auxiliary variables to avoid repeated arithmetic |
Anaesthetix | 0:0929d3d566cf | 90 | _2q0mx = 2.0f * q0 * mx; |
Anaesthetix | 0:0929d3d566cf | 91 | _2q0my = 2.0f * q0 * my; |
Anaesthetix | 0:0929d3d566cf | 92 | _2q0mz = 2.0f * q0 * mz; |
Anaesthetix | 0:0929d3d566cf | 93 | _2q1mx = 2.0f * q1 * mx; |
Anaesthetix | 0:0929d3d566cf | 94 | _2q0 = 2.0f * q0; |
Anaesthetix | 0:0929d3d566cf | 95 | _2q1 = 2.0f * q1; |
Anaesthetix | 0:0929d3d566cf | 96 | _2q2 = 2.0f * q2; |
Anaesthetix | 0:0929d3d566cf | 97 | _2q3 = 2.0f * q3; |
Anaesthetix | 0:0929d3d566cf | 98 | _2q0q2 = 2.0f * q0 * q2; |
Anaesthetix | 0:0929d3d566cf | 99 | _2q2q3 = 2.0f * q2 * q3; |
Anaesthetix | 0:0929d3d566cf | 100 | q0q0 = q0 * q0; |
Anaesthetix | 0:0929d3d566cf | 101 | q0q1 = q0 * q1; |
Anaesthetix | 0:0929d3d566cf | 102 | q0q2 = q0 * q2; |
Anaesthetix | 0:0929d3d566cf | 103 | q0q3 = q0 * q3; |
Anaesthetix | 0:0929d3d566cf | 104 | q1q1 = q1 * q1; |
Anaesthetix | 0:0929d3d566cf | 105 | q1q2 = q1 * q2; |
Anaesthetix | 0:0929d3d566cf | 106 | q1q3 = q1 * q3; |
Anaesthetix | 0:0929d3d566cf | 107 | q2q2 = q2 * q2; |
Anaesthetix | 0:0929d3d566cf | 108 | q2q3 = q2 * q3; |
Anaesthetix | 0:0929d3d566cf | 109 | q3q3 = q3 * q3; |
Anaesthetix | 5:0f4204941604 | 110 | /* |
Anaesthetix | 5:0f4204941604 | 111 | // Reference direction of Earth's magnetic field |
Anaesthetix | 5:0f4204941604 | 112 | hx = mx * q0q0 - _2q0my * q3 + _2q0mz * q2 + mx * q1q1 + _2q1 * my * q2 + _2q1 * mz * q3 - mx * q2q2 - mx * q3q3; |
Anaesthetix | 5:0f4204941604 | 113 | hy = _2q0mx * q3 + my * q0q0 - _2q0mz * q1 + _2q1mx * q2 - my * q1q1 + my * q2q2 + _2q2 * mz * q3 - my * q3q3; |
Anaesthetix | 5:0f4204941604 | 114 | _2bx = sqrtf(hx * hx + hy * hy); |
Anaesthetix | 5:0f4204941604 | 115 | _2bz = -_2q0mx * q2 + _2q0my * q1 + mz * q0q0 + _2q1mx * q3 - mz * q1q1 + _2q2 * my * q3 - mz * q2q2 + mz * q3q3; |
Anaesthetix | 5:0f4204941604 | 116 | _4bx = 2.0f * _2bx; |
Anaesthetix | 5:0f4204941604 | 117 | _4bz = 2.0f * _2bz; |
Anaesthetix | 5:0f4204941604 | 118 | |
Anaesthetix | 5:0f4204941604 | 119 | // Gradient decent algorithm corrective step |
Anaesthetix | 5:0f4204941604 | 120 | s0 = -_2q2 * (2.0f * q1q3 - _2q0q2 - ax) + _2q1 * (2.0f * q0q1 + _2q2q3 - ay) - _2bz * q2 * (_2bx * (0.5f - q2q2 - q3q3) + _2bz * (q1q3 - q0q2) - mx) + (-_2bx * q3 + _2bz * q1) * (_2bx * (q1q2 - q0q3) + _2bz * (q0q1 + q2q3) - my) + _2bx * q2 * (_2bx * (q0q2 + q1q3) + _2bz * (0.5f - q1q1 - q2q2) - mz); |
Anaesthetix | 5:0f4204941604 | 121 | s1 = _2q3 * (2.0f * q1q3 - _2q0q2 - ax) + _2q0 * (2.0f * q0q1 + _2q2q3 - ay) - 4.0f * q1 * (1 - 2.0f * q1q1 - 2.0f * q2q2 - az) + _2bz * q3 * (_2bx * (0.5f - q2q2 - q3q3) + _2bz * (q1q3 - q0q2) - mx) + (_2bx * q2 + _2bz * q0) * (_2bx * (q1q2 - q0q3) + _2bz * (q0q1 + q2q3) - my) + (_2bx * q3 - _4bz * q1) * (_2bx * (q0q2 + q1q3) + _2bz * (0.5f - q1q1 - q2q2) - mz); |
Anaesthetix | 5:0f4204941604 | 122 | s2 = -_2q0 * (2.0f * q1q3 - _2q0q2 - ax) + _2q3 * (2.0f * q0q1 + _2q2q3 - ay) - 4.0f * q2 * (1 - 2.0f * q1q1 - 2.0f * q2q2 - az) + (-_4bx * q2 - _2bz * q0) * (_2bx * (0.5f - q2q2 - q3q3) + _2bz * (q1q3 - q0q2) - mx) + (_2bx * q1 + _2bz * q3) * (_2bx * (q1q2 - q0q3) + _2bz * (q0q1 + q2q3) - my) + (_2bx * q0 - _4bz * q2) * (_2bx * (q0q2 + q1q3) + _2bz * (0.5f - q1q1 - q2q2) - mz); |
Anaesthetix | 5:0f4204941604 | 123 | s3 = _2q1 * (2.0f * q1q3 - _2q0q2 - ax) + _2q2 * (2.0f * q0q1 + _2q2q3 - ay) + (-_4bx * q3 + _2bz * q1) * (_2bx * (0.5f - q2q2 - q3q3) + _2bz * (q1q3 - q0q2) - mx) + (-_2bx * q0 + _2bz * q2) * (_2bx * (q1q2 - q0q3) + _2bz * (q0q1 + q2q3) - my) + _2bx * q1 * (_2bx * (q0q2 + q1q3) + _2bz * (0.5f - q1q1 - q2q2) - mz); |
Anaesthetix | 5:0f4204941604 | 124 | */ |
Anaesthetix | 0:0929d3d566cf | 125 | // Reference direction of Earth's magnetic field |
Anaesthetix | 0:0929d3d566cf | 126 | hx = mx * q0q0 - _2q0my * q3 + _2q0mz * q2 + mx * q1q1 + _2q1 * my * q2 + _2q1 * mz * q3 - mx * q2q2 - mx * q3q3; |
Anaesthetix | 0:0929d3d566cf | 127 | hy = _2q0mx * q3 + my * q0q0 - _2q0mz * q1 + _2q1mx * q2 - my * q1q1 + my * q2q2 + _2q2 * mz * q3 - my * q3q3; |
Anaesthetix | 5:0f4204941604 | 128 | _2bx = sqrt(hx * hx + hy * hy); |
Anaesthetix | 0:0929d3d566cf | 129 | _2bz = -_2q0mx * q2 + _2q0my * q1 + mz * q0q0 + _2q1mx * q3 - mz * q1q1 + _2q2 * my * q3 - mz * q2q2 + mz * q3q3; |
Anaesthetix | 0:0929d3d566cf | 130 | _4bx = 2.0f * _2bx; |
Anaesthetix | 0:0929d3d566cf | 131 | _4bz = 2.0f * _2bz; |
Anaesthetix | 5:0f4204941604 | 132 | _8bx = 2.0f * _4bx; |
Anaesthetix | 5:0f4204941604 | 133 | _8bz = 2.0f * _4bz; |
Anaesthetix | 0:0929d3d566cf | 134 | |
Anaesthetix | 0:0929d3d566cf | 135 | // Gradient decent algorithm corrective step |
Anaesthetix | 5:0f4204941604 | 136 | s0= -_2q2*(2.0f*(q1q3 - q0q2) - ax) + _2q1*(2.0f*(q0q1 + q2q3) - ay) + -_4bz*q2*(_4bx*(0.5 - q2q2 - q3q3) + _4bz*(q1q3 - q0q2) - mx) + (-_4bx*q3+_4bz*q1)*(_4bx*(q1q2 - q0q3) + _4bz*(q0q1 + q2q3) - my) + _4bx*q2*(_4bx*(q0q2 + q1q3) + _4bz*(0.5 - q1q1 - q2q2) - mz); |
Anaesthetix | 5:0f4204941604 | 137 | s1= _2q3*(2.0f*(q1q3 - q0q2) - ax) + _2q0*(2.0f*(q0q1 + q2q3) - ay) + -4.0f*q1*(2.0f*(0.5 - q1q1 - q2q2) - az) + _4bz*q3*(_4bx*(0.5 - q2q2 - q3q3) + _4bz*(q1q3 - q0q2) - mx) + (_4bx*q2+_4bz*q0)*(_4bx*(q1q2 - q0q3) + _4bz*(q0q1 + q2q3) - my) + (_4bx*q3-_8bz*q1)*(_4bx*(q0q2 + q1q3) + _4bz*(0.5 - q1q1 - q2q2) - mz); |
Anaesthetix | 5:0f4204941604 | 138 | s2= -_2q0*(2.0f*(q1q3 - q0q2) - ax) + _2q3*(2.0f*(q0q1 + q2q3) - ay) + (-4.0f*q2)*(2.0f*(0.5 - q1q1 - q2q2) - az) + (-_8bx*q2-_4bz*q0)*(_4bx*(0.5 - q2q2 - q3q3) + _4bz*(q1q3 - q0q2) - mx)+(_4bx*q1+_4bz*q3)*(_4bx*(q1q2 - q0q3) + _4bz*(q0q1 + q2q3) - my)+(_4bx*q0-_8bz*q2)*(_4bx*(q0q2 + q1q3) + _4bz*(0.5 - q1q1 - q2q2) - mz); |
Anaesthetix | 5:0f4204941604 | 139 | s3= _2q1*(2.0f*(q1q3 - q0q2) - ax) + _2q2*(2.0f*(q0q1 + q2q3) - ay)+(-_8bx*q3+_4bz*q1)*(_4bx*(0.5 - q2q2 - q3q3) + _4bz*(q1q3 - q0q2) - mx)+(-_4bx*q0+_4bz*q2)*(_4bx*(q1q2 - q0q3) + _4bz*(q0q1 + q2q3) - my)+(_4bx*q1)*(_4bx*(q0q2 + q1q3) + _4bz*(0.5 - q1q1 - q2q2) - mz); |
Anaesthetix | 5:0f4204941604 | 140 | recipNorm = invSqrt(s0 * s0 + s1 * s1 + s2 * s2 + s3 * s3); // normalise step magnitude |
Anaesthetix | 0:0929d3d566cf | 141 | s0 *= recipNorm; |
Anaesthetix | 0:0929d3d566cf | 142 | s1 *= recipNorm; |
Anaesthetix | 0:0929d3d566cf | 143 | s2 *= recipNorm; |
Anaesthetix | 0:0929d3d566cf | 144 | s3 *= recipNorm; |
Anaesthetix | 0:0929d3d566cf | 145 | |
Anaesthetix | 0:0929d3d566cf | 146 | // Apply feedback step |
Anaesthetix | 0:0929d3d566cf | 147 | qDot1 -= beta * s0; |
Anaesthetix | 0:0929d3d566cf | 148 | qDot2 -= beta * s1; |
Anaesthetix | 0:0929d3d566cf | 149 | qDot3 -= beta * s2; |
Anaesthetix | 0:0929d3d566cf | 150 | qDot4 -= beta * s3; |
Anaesthetix | 0:0929d3d566cf | 151 | } |
Anaesthetix | 0:0929d3d566cf | 152 | |
Anaesthetix | 0:0929d3d566cf | 153 | // Integrate rate of change of quaternion to yield quaternion |
Anaesthetix | 0:0929d3d566cf | 154 | q0 += qDot1 * invSampleFreq; |
Anaesthetix | 0:0929d3d566cf | 155 | q1 += qDot2 * invSampleFreq; |
Anaesthetix | 0:0929d3d566cf | 156 | q2 += qDot3 * invSampleFreq; |
Anaesthetix | 0:0929d3d566cf | 157 | q3 += qDot4 * invSampleFreq; |
Anaesthetix | 0:0929d3d566cf | 158 | |
Anaesthetix | 0:0929d3d566cf | 159 | // Normalise quaternion |
Anaesthetix | 0:0929d3d566cf | 160 | recipNorm = invSqrt(q0 * q0 + q1 * q1 + q2 * q2 + q3 * q3); |
Anaesthetix | 0:0929d3d566cf | 161 | q0 *= recipNorm; |
Anaesthetix | 0:0929d3d566cf | 162 | q1 *= recipNorm; |
Anaesthetix | 0:0929d3d566cf | 163 | q2 *= recipNorm; |
Anaesthetix | 0:0929d3d566cf | 164 | q3 *= recipNorm; |
Anaesthetix | 0:0929d3d566cf | 165 | anglesComputed = 0; |
Anaesthetix | 0:0929d3d566cf | 166 | } |
Anaesthetix | 0:0929d3d566cf | 167 | |
Anaesthetix | 0:0929d3d566cf | 168 | //------------------------------------------------------------------------------------------- |
Anaesthetix | 0:0929d3d566cf | 169 | // IMU algorithm update |
Anaesthetix | 0:0929d3d566cf | 170 | |
Anaesthetix | 5:0f4204941604 | 171 | void Madgwick::updateIMU(float gx, float gy, float gz, float ax, float ay, float az) |
Anaesthetix | 5:0f4204941604 | 172 | { |
Anaesthetix | 0:0929d3d566cf | 173 | float recipNorm; |
Anaesthetix | 0:0929d3d566cf | 174 | float s0, s1, s2, s3; |
Anaesthetix | 0:0929d3d566cf | 175 | float qDot1, qDot2, qDot3, qDot4; |
Anaesthetix | 0:0929d3d566cf | 176 | float _2q0, _2q1, _2q2, _2q3, _4q0, _4q1, _4q2 ,_8q1, _8q2, q0q0, q1q1, q2q2, q3q3; |
Anaesthetix | 0:0929d3d566cf | 177 | |
Anaesthetix | 0:0929d3d566cf | 178 | // Convert gyroscope degrees/sec to radians/sec |
Anaesthetix | 0:0929d3d566cf | 179 | gx *= 0.0174533f; |
Anaesthetix | 0:0929d3d566cf | 180 | gy *= 0.0174533f; |
Anaesthetix | 0:0929d3d566cf | 181 | gz *= 0.0174533f; |
Anaesthetix | 0:0929d3d566cf | 182 | |
Anaesthetix | 0:0929d3d566cf | 183 | // Rate of change of quaternion from gyroscope |
Anaesthetix | 0:0929d3d566cf | 184 | qDot1 = 0.5f * (-q1 * gx - q2 * gy - q3 * gz); |
Anaesthetix | 0:0929d3d566cf | 185 | qDot2 = 0.5f * (q0 * gx + q2 * gz - q3 * gy); |
Anaesthetix | 0:0929d3d566cf | 186 | qDot3 = 0.5f * (q0 * gy - q1 * gz + q3 * gx); |
Anaesthetix | 0:0929d3d566cf | 187 | qDot4 = 0.5f * (q0 * gz + q1 * gy - q2 * gx); |
Anaesthetix | 0:0929d3d566cf | 188 | |
Anaesthetix | 0:0929d3d566cf | 189 | // Compute feedback only if accelerometer measurement valid (avoids NaN in accelerometer normalisation) |
Anaesthetix | 0:0929d3d566cf | 190 | if(!((ax == 0.0f) && (ay == 0.0f) && (az == 0.0f))) { |
Anaesthetix | 0:0929d3d566cf | 191 | |
Anaesthetix | 0:0929d3d566cf | 192 | // Normalise accelerometer measurement |
Anaesthetix | 0:0929d3d566cf | 193 | recipNorm = invSqrt(ax * ax + ay * ay + az * az); |
Anaesthetix | 0:0929d3d566cf | 194 | ax *= recipNorm; |
Anaesthetix | 0:0929d3d566cf | 195 | ay *= recipNorm; |
Anaesthetix | 0:0929d3d566cf | 196 | az *= recipNorm; |
Anaesthetix | 0:0929d3d566cf | 197 | |
Anaesthetix | 0:0929d3d566cf | 198 | // Auxiliary variables to avoid repeated arithmetic |
Anaesthetix | 0:0929d3d566cf | 199 | _2q0 = 2.0f * q0; |
Anaesthetix | 0:0929d3d566cf | 200 | _2q1 = 2.0f * q1; |
Anaesthetix | 0:0929d3d566cf | 201 | _2q2 = 2.0f * q2; |
Anaesthetix | 0:0929d3d566cf | 202 | _2q3 = 2.0f * q3; |
Anaesthetix | 0:0929d3d566cf | 203 | _4q0 = 4.0f * q0; |
Anaesthetix | 0:0929d3d566cf | 204 | _4q1 = 4.0f * q1; |
Anaesthetix | 0:0929d3d566cf | 205 | _4q2 = 4.0f * q2; |
Anaesthetix | 0:0929d3d566cf | 206 | _8q1 = 8.0f * q1; |
Anaesthetix | 0:0929d3d566cf | 207 | _8q2 = 8.0f * q2; |
Anaesthetix | 0:0929d3d566cf | 208 | q0q0 = q0 * q0; |
Anaesthetix | 0:0929d3d566cf | 209 | q1q1 = q1 * q1; |
Anaesthetix | 0:0929d3d566cf | 210 | q2q2 = q2 * q2; |
Anaesthetix | 0:0929d3d566cf | 211 | q3q3 = q3 * q3; |
Anaesthetix | 0:0929d3d566cf | 212 | |
Anaesthetix | 0:0929d3d566cf | 213 | // Gradient decent algorithm corrective step |
Anaesthetix | 0:0929d3d566cf | 214 | s0 = _4q0 * q2q2 + _2q2 * ax + _4q0 * q1q1 - _2q1 * ay; |
Anaesthetix | 0:0929d3d566cf | 215 | s1 = _4q1 * q3q3 - _2q3 * ax + 4.0f * q0q0 * q1 - _2q0 * ay - _4q1 + _8q1 * q1q1 + _8q1 * q2q2 + _4q1 * az; |
Anaesthetix | 0:0929d3d566cf | 216 | s2 = 4.0f * q0q0 * q2 + _2q0 * ax + _4q2 * q3q3 - _2q3 * ay - _4q2 + _8q2 * q1q1 + _8q2 * q2q2 + _4q2 * az; |
Anaesthetix | 0:0929d3d566cf | 217 | s3 = 4.0f * q1q1 * q3 - _2q1 * ax + 4.0f * q2q2 * q3 - _2q2 * ay; |
Anaesthetix | 0:0929d3d566cf | 218 | recipNorm = invSqrt(s0 * s0 + s1 * s1 + s2 * s2 + s3 * s3); // normalise step magnitude |
Anaesthetix | 0:0929d3d566cf | 219 | s0 *= recipNorm; |
Anaesthetix | 0:0929d3d566cf | 220 | s1 *= recipNorm; |
Anaesthetix | 0:0929d3d566cf | 221 | s2 *= recipNorm; |
Anaesthetix | 0:0929d3d566cf | 222 | s3 *= recipNorm; |
Anaesthetix | 0:0929d3d566cf | 223 | |
Anaesthetix | 0:0929d3d566cf | 224 | // Apply feedback step |
Anaesthetix | 0:0929d3d566cf | 225 | qDot1 -= beta * s0; |
Anaesthetix | 0:0929d3d566cf | 226 | qDot2 -= beta * s1; |
Anaesthetix | 0:0929d3d566cf | 227 | qDot3 -= beta * s2; |
Anaesthetix | 0:0929d3d566cf | 228 | qDot4 -= beta * s3; |
Anaesthetix | 0:0929d3d566cf | 229 | } |
Anaesthetix | 0:0929d3d566cf | 230 | |
Anaesthetix | 0:0929d3d566cf | 231 | // Integrate rate of change of quaternion to yield quaternion |
Anaesthetix | 0:0929d3d566cf | 232 | q0 += qDot1 * invSampleFreq; |
Anaesthetix | 0:0929d3d566cf | 233 | q1 += qDot2 * invSampleFreq; |
Anaesthetix | 0:0929d3d566cf | 234 | q2 += qDot3 * invSampleFreq; |
Anaesthetix | 0:0929d3d566cf | 235 | q3 += qDot4 * invSampleFreq; |
Anaesthetix | 0:0929d3d566cf | 236 | |
Anaesthetix | 0:0929d3d566cf | 237 | // Normalise quaternion |
Anaesthetix | 0:0929d3d566cf | 238 | recipNorm = invSqrt(q0 * q0 + q1 * q1 + q2 * q2 + q3 * q3); |
Anaesthetix | 0:0929d3d566cf | 239 | q0 *= recipNorm; |
Anaesthetix | 0:0929d3d566cf | 240 | q1 *= recipNorm; |
Anaesthetix | 0:0929d3d566cf | 241 | q2 *= recipNorm; |
Anaesthetix | 0:0929d3d566cf | 242 | q3 *= recipNorm; |
Anaesthetix | 0:0929d3d566cf | 243 | anglesComputed = 0; |
Anaesthetix | 0:0929d3d566cf | 244 | } |
Anaesthetix | 0:0929d3d566cf | 245 | |
Anaesthetix | 0:0929d3d566cf | 246 | //------------------------------------------------------------------------------------------- |
Anaesthetix | 0:0929d3d566cf | 247 | // Fast inverse square-root |
Anaesthetix | 0:0929d3d566cf | 248 | // See: http://en.wikipedia.org/wiki/Fast_inverse_square_root |
Anaesthetix | 0:0929d3d566cf | 249 | |
Anaesthetix | 0:0929d3d566cf | 250 | /*float Madgwick::invSqrt(float x) { |
Anaesthetix | 0:0929d3d566cf | 251 | float halfx = 0.5f * x; |
Anaesthetix | 0:0929d3d566cf | 252 | float y = x; |
Anaesthetix | 0:0929d3d566cf | 253 | long i = *(long*)&y; |
Anaesthetix | 0:0929d3d566cf | 254 | i = 0x5f3759df - (i>>1); |
Anaesthetix | 0:0929d3d566cf | 255 | y = *(float*)&i; |
Anaesthetix | 0:0929d3d566cf | 256 | y = y * (1.5f - (halfx * y * y)); |
Anaesthetix | 0:0929d3d566cf | 257 | y = y * (1.5f - (halfx * y * y)); |
Anaesthetix | 0:0929d3d566cf | 258 | return y; |
Anaesthetix | 5:0f4204941604 | 259 | } |
Anaesthetix | 0:0929d3d566cf | 260 | |
Anaesthetix | 0:0929d3d566cf | 261 | float Madgwick::invSqrt(float x){ |
Anaesthetix | 0:0929d3d566cf | 262 | unsigned int i = 0x5F1F1412 - (*(unsigned int*)&x >> 1); |
Anaesthetix | 0:0929d3d566cf | 263 | float tmp = *(float*)&i; |
Anaesthetix | 0:0929d3d566cf | 264 | return tmp * (1.69000231f - 0.714158168f * x * tmp * tmp); |
Anaesthetix | 0:0929d3d566cf | 265 | } |
Anaesthetix | 0:0929d3d566cf | 266 | */ |
Anaesthetix | 5:0f4204941604 | 267 | float Madgwick::invSqrt(float x) |
Anaesthetix | 5:0f4204941604 | 268 | { |
Anaesthetix | 5:0f4204941604 | 269 | float tmp = 1/(sqrt(x)); |
Anaesthetix | 5:0f4204941604 | 270 | return tmp; |
Anaesthetix | 0:0929d3d566cf | 271 | } |
Anaesthetix | 0:0929d3d566cf | 272 | |
Anaesthetix | 0:0929d3d566cf | 273 | //------------------------------------------------------------------------------------------- |
Anaesthetix | 0:0929d3d566cf | 274 | |
Anaesthetix | 0:0929d3d566cf | 275 | void Madgwick::computeAngles() |
Anaesthetix | 0:0929d3d566cf | 276 | { |
Anaesthetix | 0:0929d3d566cf | 277 | roll = atan2f(q0*q1 + q2*q3, 0.5f - q1*q1 - q2*q2); |
Anaesthetix | 0:0929d3d566cf | 278 | pitch = asinf(-2.0f * (q1*q3 - q0*q2)); |
Anaesthetix | 0:0929d3d566cf | 279 | yaw = atan2f(q1*q2 + q0*q3, 0.5f - q2*q2 - q3*q3); |
Anaesthetix | 0:0929d3d566cf | 280 | anglesComputed = 1; |
Anaesthetix | 0:0929d3d566cf | 281 | } |
Anaesthetix | 0:0929d3d566cf | 282 |