IMU filter
MadgwickAHRS.cpp@0:0c61d7209f75, 2016-05-30 (annotated)
- Committer:
- Decimus
- Date:
- Mon May 30 08:10:20 2016 +0000
- Revision:
- 0:0c61d7209f75
[+]
Who changed what in which revision?
User | Revision | Line number | New contents of line |
---|---|---|---|
Decimus | 0:0c61d7209f75 | 1 | |
Decimus | 0:0c61d7209f75 | 2 | // MadgwickAHRS.c |
Decimus | 0:0c61d7209f75 | 3 | //===================================================================================================== |
Decimus | 0:0c61d7209f75 | 4 | // |
Decimus | 0:0c61d7209f75 | 5 | // Implementation of Madgwick's IMU and AHRS algorithms. |
Decimus | 0:0c61d7209f75 | 6 | // See: http://www.x-io.co.uk/node/8#open_source_ahrs_and_imu_algorithms |
Decimus | 0:0c61d7209f75 | 7 | // |
Decimus | 0:0c61d7209f75 | 8 | // Date Author Notes |
Decimus | 0:0c61d7209f75 | 9 | // 29/09/2011 SOH Madgwick Initial release |
Decimus | 0:0c61d7209f75 | 10 | // 02/10/2011 SOH Madgwick Optimised for reduced CPU load |
Decimus | 0:0c61d7209f75 | 11 | // 19/02/2012 SOH Madgwick Magnetometer measurement is normalised |
Decimus | 0:0c61d7209f75 | 12 | // |
Decimus | 0:0c61d7209f75 | 13 | //===================================================================================================== |
Decimus | 0:0c61d7209f75 | 14 | |
Decimus | 0:0c61d7209f75 | 15 | //--------------------------------------------------------------------------------------------------- |
Decimus | 0:0c61d7209f75 | 16 | // Header files |
Decimus | 0:0c61d7209f75 | 17 | |
Decimus | 0:0c61d7209f75 | 18 | #include "MadgwickAHRS.h" |
Decimus | 0:0c61d7209f75 | 19 | #include <math.h> |
Decimus | 0:0c61d7209f75 | 20 | |
Decimus | 0:0c61d7209f75 | 21 | //--------------------------------------------------------------------------------------------------- |
Decimus | 0:0c61d7209f75 | 22 | // Definitions |
Decimus | 0:0c61d7209f75 | 23 | |
Decimus | 0:0c61d7209f75 | 24 | #define sampleFreq 512.0f // sample frequency in Hz |
Decimus | 0:0c61d7209f75 | 25 | #define betaDef 0.1f // 2 * proportional gain |
Decimus | 0:0c61d7209f75 | 26 | |
Decimus | 0:0c61d7209f75 | 27 | //--------------------------------------------------------------------------------------------------- |
Decimus | 0:0c61d7209f75 | 28 | // Variable definitions |
Decimus | 0:0c61d7209f75 | 29 | |
Decimus | 0:0c61d7209f75 | 30 | volatile float beta = betaDef; // 2 * proportional gain (Kp) |
Decimus | 0:0c61d7209f75 | 31 | volatile float q0 = 1.0f, q1 = 0.0f, q2 = 0.0f, q3 = 0.0f; // quaternion of sensor frame relative to auxiliary frame |
Decimus | 0:0c61d7209f75 | 32 | //volatile float quat[4]; |
Decimus | 0:0c61d7209f75 | 33 | |
Decimus | 0:0c61d7209f75 | 34 | //==================================================================================================== |
Decimus | 0:0c61d7209f75 | 35 | // Functions |
Decimus | 0:0c61d7209f75 | 36 | |
Decimus | 0:0c61d7209f75 | 37 | //--------------------------------------------------------------------------------------------------- |
Decimus | 0:0c61d7209f75 | 38 | // AHRS algorithm update |
Decimus | 0:0c61d7209f75 | 39 | |
Decimus | 0:0c61d7209f75 | 40 | void MadgwickAHRSupdate(float tdelta, float gx, float gy, float gz, float ax, float ay, float az, float mx, float my, float mz) { |
Decimus | 0:0c61d7209f75 | 41 | float recipNorm; |
Decimus | 0:0c61d7209f75 | 42 | float s0, s1, s2, s3; |
Decimus | 0:0c61d7209f75 | 43 | float qDot1, qDot2, qDot3, qDot4; |
Decimus | 0:0c61d7209f75 | 44 | float hx, hy; |
Decimus | 0:0c61d7209f75 | 45 | float _2q0mx, _2q0my, _2q0mz, _2q1mx, _2bx, _2bz, _4bx, _4bz, _2q0, _2q1, _2q2, _2q3, _2q0q2, _2q2q3, q0q0, q0q1, q0q2, q0q3, q1q1, q1q2, q1q3, q2q2, q2q3, q3q3; |
Decimus | 0:0c61d7209f75 | 46 | |
Decimus | 0:0c61d7209f75 | 47 | // Use IMU algorithm if magnetometer measurement invalid (avoids NaN in magnetometer normalisation) |
Decimus | 0:0c61d7209f75 | 48 | if((mx == 0.0f) && (my == 0.0f) && (mz == 0.0f)) { |
Decimus | 0:0c61d7209f75 | 49 | MadgwickAHRSupdateIMU( tdelta, gx, gy, gz, ax, ay, az); |
Decimus | 0:0c61d7209f75 | 50 | return; |
Decimus | 0:0c61d7209f75 | 51 | } |
Decimus | 0:0c61d7209f75 | 52 | |
Decimus | 0:0c61d7209f75 | 53 | // Rate of change of quaternion from gyroscope |
Decimus | 0:0c61d7209f75 | 54 | qDot1 = 0.5f * (-q1 * gx - q2 * gy - q3 * gz); |
Decimus | 0:0c61d7209f75 | 55 | qDot2 = 0.5f * (q0 * gx + q2 * gz - q3 * gy); |
Decimus | 0:0c61d7209f75 | 56 | qDot3 = 0.5f * (q0 * gy - q1 * gz + q3 * gx); |
Decimus | 0:0c61d7209f75 | 57 | qDot4 = 0.5f * (q0 * gz + q1 * gy - q2 * gx); |
Decimus | 0:0c61d7209f75 | 58 | |
Decimus | 0:0c61d7209f75 | 59 | // Compute feedback only if accelerometer measurement valid (avoids NaN in accelerometer normalisation) |
Decimus | 0:0c61d7209f75 | 60 | if(!((ax == 0.0f) && (ay == 0.0f) && (az == 0.0f))) { |
Decimus | 0:0c61d7209f75 | 61 | |
Decimus | 0:0c61d7209f75 | 62 | // Normalise accelerometer measurement |
Decimus | 0:0c61d7209f75 | 63 | recipNorm = invSqrt(ax * ax + ay * ay + az * az); |
Decimus | 0:0c61d7209f75 | 64 | ax *= recipNorm; |
Decimus | 0:0c61d7209f75 | 65 | ay *= recipNorm; |
Decimus | 0:0c61d7209f75 | 66 | az *= recipNorm; |
Decimus | 0:0c61d7209f75 | 67 | |
Decimus | 0:0c61d7209f75 | 68 | // Normalise magnetometer measurement |
Decimus | 0:0c61d7209f75 | 69 | recipNorm = invSqrt(mx * mx + my * my + mz * mz); |
Decimus | 0:0c61d7209f75 | 70 | mx *= recipNorm; |
Decimus | 0:0c61d7209f75 | 71 | my *= recipNorm; |
Decimus | 0:0c61d7209f75 | 72 | mz *= recipNorm; |
Decimus | 0:0c61d7209f75 | 73 | |
Decimus | 0:0c61d7209f75 | 74 | // Auxiliary variables to avoid repeated arithmetic |
Decimus | 0:0c61d7209f75 | 75 | _2q0mx = 2.0f * q0 * mx; |
Decimus | 0:0c61d7209f75 | 76 | _2q0my = 2.0f * q0 * my; |
Decimus | 0:0c61d7209f75 | 77 | _2q0mz = 2.0f * q0 * mz; |
Decimus | 0:0c61d7209f75 | 78 | _2q1mx = 2.0f * q1 * mx; |
Decimus | 0:0c61d7209f75 | 79 | _2q0 = 2.0f * q0; |
Decimus | 0:0c61d7209f75 | 80 | _2q1 = 2.0f * q1; |
Decimus | 0:0c61d7209f75 | 81 | _2q2 = 2.0f * q2; |
Decimus | 0:0c61d7209f75 | 82 | _2q3 = 2.0f * q3; |
Decimus | 0:0c61d7209f75 | 83 | _2q0q2 = 2.0f * q0 * q2; |
Decimus | 0:0c61d7209f75 | 84 | _2q2q3 = 2.0f * q2 * q3; |
Decimus | 0:0c61d7209f75 | 85 | q0q0 = q0 * q0; |
Decimus | 0:0c61d7209f75 | 86 | q0q1 = q0 * q1; |
Decimus | 0:0c61d7209f75 | 87 | q0q2 = q0 * q2; |
Decimus | 0:0c61d7209f75 | 88 | q0q3 = q0 * q3; |
Decimus | 0:0c61d7209f75 | 89 | q1q1 = q1 * q1; |
Decimus | 0:0c61d7209f75 | 90 | q1q2 = q1 * q2; |
Decimus | 0:0c61d7209f75 | 91 | q1q3 = q1 * q3; |
Decimus | 0:0c61d7209f75 | 92 | q2q2 = q2 * q2; |
Decimus | 0:0c61d7209f75 | 93 | q2q3 = q2 * q3; |
Decimus | 0:0c61d7209f75 | 94 | q3q3 = q3 * q3; |
Decimus | 0:0c61d7209f75 | 95 | |
Decimus | 0:0c61d7209f75 | 96 | // Reference direction of Earth's magnetic field |
Decimus | 0:0c61d7209f75 | 97 | hx = mx * q0q0 - _2q0my * q3 + _2q0mz * q2 + mx * q1q1 + _2q1 * my * q2 + _2q1 * mz * q3 - mx * q2q2 - mx * q3q3; |
Decimus | 0:0c61d7209f75 | 98 | hy = _2q0mx * q3 + my * q0q0 - _2q0mz * q1 + _2q1mx * q2 - my * q1q1 + my * q2q2 + _2q2 * mz * q3 - my * q3q3; |
Decimus | 0:0c61d7209f75 | 99 | _2bx = sqrt(hx * hx + hy * hy); |
Decimus | 0:0c61d7209f75 | 100 | _2bz = -_2q0mx * q2 + _2q0my * q1 + mz * q0q0 + _2q1mx * q3 - mz * q1q1 + _2q2 * my * q3 - mz * q2q2 + mz * q3q3; |
Decimus | 0:0c61d7209f75 | 101 | _4bx = 2.0f * _2bx; |
Decimus | 0:0c61d7209f75 | 102 | _4bz = 2.0f * _2bz; |
Decimus | 0:0c61d7209f75 | 103 | |
Decimus | 0:0c61d7209f75 | 104 | // Gradient decent algorithm corrective step |
Decimus | 0:0c61d7209f75 | 105 | 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); |
Decimus | 0:0c61d7209f75 | 106 | 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); |
Decimus | 0:0c61d7209f75 | 107 | 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); |
Decimus | 0:0c61d7209f75 | 108 | 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); |
Decimus | 0:0c61d7209f75 | 109 | recipNorm = invSqrt(s0 * s0 + s1 * s1 + s2 * s2 + s3 * s3); // normalise step magnitude |
Decimus | 0:0c61d7209f75 | 110 | s0 *= recipNorm; |
Decimus | 0:0c61d7209f75 | 111 | s1 *= recipNorm; |
Decimus | 0:0c61d7209f75 | 112 | s2 *= recipNorm; |
Decimus | 0:0c61d7209f75 | 113 | s3 *= recipNorm; |
Decimus | 0:0c61d7209f75 | 114 | |
Decimus | 0:0c61d7209f75 | 115 | // Apply feedback step |
Decimus | 0:0c61d7209f75 | 116 | qDot1 -= beta * s0; |
Decimus | 0:0c61d7209f75 | 117 | qDot2 -= beta * s1; |
Decimus | 0:0c61d7209f75 | 118 | qDot3 -= beta * s2; |
Decimus | 0:0c61d7209f75 | 119 | qDot4 -= beta * s3; |
Decimus | 0:0c61d7209f75 | 120 | } |
Decimus | 0:0c61d7209f75 | 121 | |
Decimus | 0:0c61d7209f75 | 122 | // Integrate rate of change of quaternion to yield quaternion |
Decimus | 0:0c61d7209f75 | 123 | q0 += qDot1 * tdelta; |
Decimus | 0:0c61d7209f75 | 124 | q1 += qDot2 * tdelta; |
Decimus | 0:0c61d7209f75 | 125 | q2 += qDot3 * tdelta; |
Decimus | 0:0c61d7209f75 | 126 | q3 += qDot4 * tdelta; |
Decimus | 0:0c61d7209f75 | 127 | |
Decimus | 0:0c61d7209f75 | 128 | // Normalise quaternion |
Decimus | 0:0c61d7209f75 | 129 | recipNorm = invSqrt(q0 * q0 + q1 * q1 + q2 * q2 + q3 * q3); |
Decimus | 0:0c61d7209f75 | 130 | q0 *= recipNorm; |
Decimus | 0:0c61d7209f75 | 131 | q1 *= recipNorm; |
Decimus | 0:0c61d7209f75 | 132 | q2 *= recipNorm; |
Decimus | 0:0c61d7209f75 | 133 | q3 *= recipNorm; |
Decimus | 0:0c61d7209f75 | 134 | } |
Decimus | 0:0c61d7209f75 | 135 | |
Decimus | 0:0c61d7209f75 | 136 | //--------------------------------------------------------------------------------------------------- |
Decimus | 0:0c61d7209f75 | 137 | // IMU algorithm update |
Decimus | 0:0c61d7209f75 | 138 | |
Decimus | 0:0c61d7209f75 | 139 | void MadgwickAHRSupdateIMU(float tdelta, float gx, float gy, float gz, float ax, float ay, float az) { |
Decimus | 0:0c61d7209f75 | 140 | float recipNorm; |
Decimus | 0:0c61d7209f75 | 141 | float s0, s1, s2, s3; |
Decimus | 0:0c61d7209f75 | 142 | float qDot1, qDot2, qDot3, qDot4; |
Decimus | 0:0c61d7209f75 | 143 | float _2q0, _2q1, _2q2, _2q3, _4q0, _4q1, _4q2 ,_8q1, _8q2, q0q0, q1q1, q2q2, q3q3; |
Decimus | 0:0c61d7209f75 | 144 | |
Decimus | 0:0c61d7209f75 | 145 | // Rate of change of quaternion from gyroscope |
Decimus | 0:0c61d7209f75 | 146 | qDot1 = 0.5f * (-q1 * gx - q2 * gy - q3 * gz); |
Decimus | 0:0c61d7209f75 | 147 | qDot2 = 0.5f * (q0 * gx + q2 * gz - q3 * gy); |
Decimus | 0:0c61d7209f75 | 148 | qDot3 = 0.5f * (q0 * gy - q1 * gz + q3 * gx); |
Decimus | 0:0c61d7209f75 | 149 | qDot4 = 0.5f * (q0 * gz + q1 * gy - q2 * gx); |
Decimus | 0:0c61d7209f75 | 150 | |
Decimus | 0:0c61d7209f75 | 151 | // Compute feedback only if accelerometer measurement valid (avoids NaN in accelerometer normalisation) |
Decimus | 0:0c61d7209f75 | 152 | if(!((ax == 0.0f) && (ay == 0.0f) && (az == 0.0f))) { |
Decimus | 0:0c61d7209f75 | 153 | // Normalise accelerometer measurement |
Decimus | 0:0c61d7209f75 | 154 | recipNorm = invSqrt(ax * ax + ay * ay + az * az); |
Decimus | 0:0c61d7209f75 | 155 | ax *= recipNorm; |
Decimus | 0:0c61d7209f75 | 156 | ay *= recipNorm; |
Decimus | 0:0c61d7209f75 | 157 | az *= recipNorm; |
Decimus | 0:0c61d7209f75 | 158 | |
Decimus | 0:0c61d7209f75 | 159 | // Auxiliary variables to avoid repeated arithmetic |
Decimus | 0:0c61d7209f75 | 160 | _2q0 = 2.0f * q0; |
Decimus | 0:0c61d7209f75 | 161 | _2q1 = 2.0f * q1; |
Decimus | 0:0c61d7209f75 | 162 | _2q2 = 2.0f * q2; |
Decimus | 0:0c61d7209f75 | 163 | _2q3 = 2.0f * q3; |
Decimus | 0:0c61d7209f75 | 164 | _4q0 = 4.0f * q0; |
Decimus | 0:0c61d7209f75 | 165 | _4q1 = 4.0f * q1; |
Decimus | 0:0c61d7209f75 | 166 | _4q2 = 4.0f * q2; |
Decimus | 0:0c61d7209f75 | 167 | _8q1 = 8.0f * q1; |
Decimus | 0:0c61d7209f75 | 168 | _8q2 = 8.0f * q2; |
Decimus | 0:0c61d7209f75 | 169 | q0q0 = q0 * q0; |
Decimus | 0:0c61d7209f75 | 170 | q1q1 = q1 * q1; |
Decimus | 0:0c61d7209f75 | 171 | q2q2 = q2 * q2; |
Decimus | 0:0c61d7209f75 | 172 | q3q3 = q3 * q3; |
Decimus | 0:0c61d7209f75 | 173 | |
Decimus | 0:0c61d7209f75 | 174 | // Gradient decent algorithm corrective step |
Decimus | 0:0c61d7209f75 | 175 | s0 = _4q0 * q2q2 + _2q2 * ax + _4q0 * q1q1 - _2q1 * ay; |
Decimus | 0:0c61d7209f75 | 176 | s1 = _4q1 * q3q3 - _2q3 * ax + 4.0f * q0q0 * q1 - _2q0 * ay - _4q1 + _8q1 * q1q1 + _8q1 * q2q2 + _4q1 * az; |
Decimus | 0:0c61d7209f75 | 177 | s2 = 4.0f * q0q0 * q2 + _2q0 * ax + _4q2 * q3q3 - _2q3 * ay - _4q2 + _8q2 * q1q1 + _8q2 * q2q2 + _4q2 * az; |
Decimus | 0:0c61d7209f75 | 178 | s3 = 4.0f * q1q1 * q3 - _2q1 * ax + 4.0f * q2q2 * q3 - _2q2 * ay; |
Decimus | 0:0c61d7209f75 | 179 | recipNorm = invSqrt(s0 * s0 + s1 * s1 + s2 * s2 + s3 * s3); // normalise step magnitude |
Decimus | 0:0c61d7209f75 | 180 | s0 *= recipNorm; |
Decimus | 0:0c61d7209f75 | 181 | s1 *= recipNorm; |
Decimus | 0:0c61d7209f75 | 182 | s2 *= recipNorm; |
Decimus | 0:0c61d7209f75 | 183 | s3 *= recipNorm; |
Decimus | 0:0c61d7209f75 | 184 | // Apply feedback step |
Decimus | 0:0c61d7209f75 | 185 | qDot1 -= beta * s0; |
Decimus | 0:0c61d7209f75 | 186 | qDot2 -= beta * s1; |
Decimus | 0:0c61d7209f75 | 187 | qDot3 -= beta * s2; |
Decimus | 0:0c61d7209f75 | 188 | qDot4 -= beta * s3; |
Decimus | 0:0c61d7209f75 | 189 | } |
Decimus | 0:0c61d7209f75 | 190 | |
Decimus | 0:0c61d7209f75 | 191 | // Integrate rate of change of quaternion to yield quaternion |
Decimus | 0:0c61d7209f75 | 192 | q0 += qDot1 * tdelta; |
Decimus | 0:0c61d7209f75 | 193 | q1 += qDot2 * tdelta; |
Decimus | 0:0c61d7209f75 | 194 | q2 += qDot3 * tdelta; |
Decimus | 0:0c61d7209f75 | 195 | q3 += qDot4 * tdelta; |
Decimus | 0:0c61d7209f75 | 196 | |
Decimus | 0:0c61d7209f75 | 197 | // Normalise quaternion |
Decimus | 0:0c61d7209f75 | 198 | recipNorm = invSqrt(q0 * q0 + q1 * q1 + q2 * q2 + q3 * q3); |
Decimus | 0:0c61d7209f75 | 199 | q0 *= recipNorm; |
Decimus | 0:0c61d7209f75 | 200 | q1 *= recipNorm; |
Decimus | 0:0c61d7209f75 | 201 | q2 *= recipNorm; |
Decimus | 0:0c61d7209f75 | 202 | q3 *= recipNorm; |
Decimus | 0:0c61d7209f75 | 203 | //quat[0] = q0; |
Decimus | 0:0c61d7209f75 | 204 | //quat[1] = q1; |
Decimus | 0:0c61d7209f75 | 205 | //quat[2] = q2; |
Decimus | 0:0c61d7209f75 | 206 | //quat[3] = q3; |
Decimus | 0:0c61d7209f75 | 207 | } |
Decimus | 0:0c61d7209f75 | 208 | |
Decimus | 0:0c61d7209f75 | 209 | |
Decimus | 0:0c61d7209f75 | 210 | int instability_fix = 1; |
Decimus | 0:0c61d7209f75 | 211 | |
Decimus | 0:0c61d7209f75 | 212 | //--------------------------------------------------------------------------------------------------- |
Decimus | 0:0c61d7209f75 | 213 | // Fast inverse square-root |
Decimus | 0:0c61d7209f75 | 214 | // See: http://en.wikipedia.org/wiki/Fast_inverse_square_root |
Decimus | 0:0c61d7209f75 | 215 | |
Decimus | 0:0c61d7209f75 | 216 | float invSqrt(float x) { |
Decimus | 0:0c61d7209f75 | 217 | if (instability_fix == 0) |
Decimus | 0:0c61d7209f75 | 218 | { |
Decimus | 0:0c61d7209f75 | 219 | /* original code */ |
Decimus | 0:0c61d7209f75 | 220 | float halfx = 0.5f * x; |
Decimus | 0:0c61d7209f75 | 221 | float y = x; |
Decimus | 0:0c61d7209f75 | 222 | long i = *(long*)&y; |
Decimus | 0:0c61d7209f75 | 223 | i = 0x5f3759df - (i>>1); |
Decimus | 0:0c61d7209f75 | 224 | y = *(float*)&i; |
Decimus | 0:0c61d7209f75 | 225 | y = y * (1.5f - (halfx * y * y)); |
Decimus | 0:0c61d7209f75 | 226 | return y; |
Decimus | 0:0c61d7209f75 | 227 | } |
Decimus | 0:0c61d7209f75 | 228 | else if (instability_fix == 1) |
Decimus | 0:0c61d7209f75 | 229 | { |
Decimus | 0:0c61d7209f75 | 230 | /* close-to-optimal method with low cost from http://pizer.wordpress.com/2008/10/12/fast-inverse-square-root */ |
Decimus | 0:0c61d7209f75 | 231 | unsigned int i = 0x5F1F1412 - (*(unsigned int*)&x >> 1); |
Decimus | 0:0c61d7209f75 | 232 | float tmp = *(float*)&i; |
Decimus | 0:0c61d7209f75 | 233 | return tmp * (1.69000231f - 0.714158168f * x * tmp * tmp); |
Decimus | 0:0c61d7209f75 | 234 | } |
Decimus | 0:0c61d7209f75 | 235 | else |
Decimus | 0:0c61d7209f75 | 236 | { |
Decimus | 0:0c61d7209f75 | 237 | /* optimal but expensive method: */ |
Decimus | 0:0c61d7209f75 | 238 | return 1.0f / sqrtf(x); |
Decimus | 0:0c61d7209f75 | 239 | } |
Decimus | 0:0c61d7209f75 | 240 | } |
Decimus | 0:0c61d7209f75 | 241 | |
Decimus | 0:0c61d7209f75 | 242 | //==================================================================================================== |
Decimus | 0:0c61d7209f75 | 243 | // END OF CODE |
Decimus | 0:0c61d7209f75 | 244 | //==================================================================================================== |