//=====================================================================================================
// MahonyAHRS.c
//=====================================================================================================
//
// Madgwick's implementation of Mayhony's AHRS algorithm.
// See: http://www.x-io.co.uk/node/8#open_source_ahrs_and_imu_algorithms
//
// Date			Author			Notes
// 29/09/2011	SOH Madgwick    Initial release
// 02/10/2011	SOH Madgwick	Optimised for reduced CPU load
//
//=====================================================================================================

//---------------------------------------------------------------------------------------------------
// Header files

#include "MahonyAHRS.h"
#include "Arduino.h"
#include <math.h>
//---------------------------------------------------------------------------------------------------
// Definitions

#define sampleFreq	25.0f			// sample frequency in Hz
#define twoKpDef	(2.0f * 1.0f)	// 2 * proportional gain
#define twoKiDef	(2.0f * 0.0f)	// 2 * integral gain

//#define twoKiDef	(0.0f * 0.0f)

//---------------------------------------------------------------------------------------------------
// Variable definitions

volatile float twoKp = twoKpDef;											// 2 * proportional gain (Kp)
volatile float twoKi = twoKiDef;											// 2 * integral gain (Ki)
volatile float q0 = 1.0, q1 = 0.0, q2 = 0.0, q3 = 0.0;					// quaternion of sensor frame relative to auxiliary frame
volatile float integralFBx = 0.0f,  integralFBy = 0.0f, integralFBz = 0.0f;	// integral error terms scaled by Ki

//---------------------------------------------------------------------------------------------------
// Function declarations

//float invSqrt(float x);

//====================================================================================================
// Functions

//---------------------------------------------------------------------------------------------------
// AHRS algorithm update

void MahonyAHRSupdate(float gx, float gy, float gz, float ax, float ay, float az, float mx, float my, float mz) {
	float recipNorm;
    float q0q0, q0q1, q0q2, q0q3, q1q1, q1q2, q1q3, q2q2, q2q3, q3q3;
	float hx, hy, bx, bz;
	float halfvx, halfvy, halfvz, halfwx, halfwy, halfwz;
	float halfex, halfey, halfez;
	float qa, qb, qc;

	// Use IMU algorithm if magnetometer measurement invalid (avoids NaN in magnetometer normalisation)
	if((mx == 0.0f) && (my == 0.0f) && (mz == 0.0f)) {
		//MahonyAHRSupdateIMU(gx, gy, gz, ax, ay, az);
		return;
	}

	// Compute feedback only if accelerometer measurement valid (avoids NaN in accelerometer normalisation)
	if(!((ax == 0.0f) && (ay == 0.0f) && (az == 0.0f))) {

		// Normalise accelerometer measurement
		recipNorm = sqrt(ax * ax + ay * ay + az * az);
		ax *= recipNorm;
		ay *= recipNorm;
		az *= recipNorm;

		// Normalise magnetometer measurement
		recipNorm = sqrt(mx * mx + my * my + mz * mz);
		mx *= recipNorm;
		my *= recipNorm;
		mz *= recipNorm;

        // Auxiliary variables to avoid repeated arithmetic
        q0q0 = q0 * q0;
        q0q1 = q0 * q1;
        q0q2 = q0 * q2;
        q0q3 = q0 * q3;
        q1q1 = q1 * q1;
        q1q2 = q1 * q2;
        q1q3 = q1 * q3;
        q2q2 = q2 * q2;
        q2q3 = q2 * q3;
        q3q3 = q3 * q3;

        // Reference direction of Earth's magnetic field
        hx = 2.0f * (mx * (0.5f - q2q2 - q3q3) + my * (q1q2 - q0q3) + mz * (q1q3 + q0q2));
        hy = 2.0f * (mx * (q1q2 + q0q3) + my * (0.5f - q1q1 - q3q3) + mz * (q2q3 - q0q1));
        bx = sqrt(hx * hx + hy * hy);
        bz = 2.0f * (mx * (q1q3 - q0q2) + my * (q2q3 + q0q1) + mz * (0.5f - q1q1 - q2q2));

		// Estimated direction of gravity and magnetic field
		halfvx = q1q3 - q0q2;
		halfvy = q0q1 + q2q3;
		halfvz = q0q0 - 0.5f + q3q3;
        halfwx = bx * (0.5f - q2q2 - q3q3) + bz * (q1q3 - q0q2);
        halfwy = bx * (q1q2 - q0q3) + bz * (q0q1 + q2q3);
        halfwz = bx * (q0q2 + q1q3) + bz * (0.5f - q1q1 - q2q2);

		// Error is sum of cross product between estimated direction and measured direction of field vectors
		halfex = (ay * halfvz - az * halfvy) + (my * halfwz - mz * halfwy);
		halfey = (az * halfvx - ax * halfvz) + (mz * halfwx - mx * halfwz);
		halfez = (ax * halfvy - ay * halfvx) + (mx * halfwy - my * halfwx);

		// Compute and apply integral feedback if enabled
		if(twoKi > 0.0f) {
			integralFBx += twoKi * halfex * (1.0f / sampleFreq);	// integral error scaled by Ki
			integralFBy += twoKi * halfey * (1.0f / sampleFreq);
			integralFBz += twoKi * halfez * (1.0f / sampleFreq);
			gx += integralFBx;	// apply integral feedback
			gy += integralFBy;
			gz += integralFBz;
		}
		else {
			integralFBx = 0.0f;	// prevent integral windup
			integralFBy = 0.0f;
			integralFBz = 0.0f;
		}

		// Apply proportional feedback
		gx += twoKp * halfex;
		gy += twoKp * halfey;
		gz += twoKp * halfez;
	}

	// Integrate rate of change of quaternion
	gx *= (0.5f * (1.0f / sampleFreq));		// pre-multiply common factors
	gy *= (0.5f * (1.0f / sampleFreq));
	gz *= (0.5f * (1.0f / sampleFreq));
	qa = q0;
	qb = q1;
	qc = q2;
	q0 += (-qb * gx - qc * gy - q3 * gz);
	q1 += (qa * gx + qc * gz - q3 * gy);
	q2 += (qa * gy - qb * gz + q3 * gx);
	q3 += (qa * gz + qb * gy - qc * gx);

	// Normalise quaternion
	recipNorm = sqrt(q0 * q0 + q1 * q1 + q2 * q2 + q3 * q3);
	q0 *= recipNorm;
	q1 *= recipNorm;
	q2 *= recipNorm;
	q3 *= recipNorm;
}

//---------------------------------------------------------------------------------------------------
// IMU algorithm update

void MahonyAHRSupdateIMU(float gx, float gy, float gz, float ax, float ay, float az,float *pitch,float *roll,float *yaw) {
	float recipNorm;
	float halfvx, halfvy, halfvz;
	float halfex, halfey, halfez;
	float qa, qb, qc;


	// Compute feedback only if accelerometer measurement valid (avoids NaN in accelerometer normalisation)
	if(!((ax == 0.0f) && (ay == 0.0f) && (az == 0.0f))) {

		// Normalise accelerometer measurement
		recipNorm = invSqrt(ax * ax + ay * ay + az * az);
		ax *= recipNorm;
		ay *= recipNorm;
		az *= recipNorm;

		// Estimated direction of gravity and vector perpendicular to magnetic flux
		halfvx = q1 * q3 - q0 * q2;
		halfvy = q0 * q1 + q2 * q3;
		halfvz = q0 * q0 - 0.5f + q3 * q3;

		

		// Error is sum of cross product between estimated and measured direction of gravity
		halfex = (ay * halfvz - az * halfvy);
		halfey = (az * halfvx - ax * halfvz);
		halfez = (ax * halfvy - ay * halfvx);

		// Compute and apply integral feedback if enabled
		if(twoKi > 0.0f) {
			integralFBx += twoKi * halfex * (1.0f / sampleFreq);	// integral error scaled by Ki
			integralFBy += twoKi * halfey * (1.0f / sampleFreq);
			integralFBz += twoKi * halfez * (1.0f / sampleFreq);
			gx += integralFBx;	// apply integral feedback
			gy += integralFBy;
			gz += integralFBz;
		}
		else {
			integralFBx = 0.0f;	// prevent integral windup
			integralFBy = 0.0f;
			integralFBz = 0.0f;
		}

		// Apply proportional feedback
		gx += twoKp * halfex;
		gy += twoKp * halfey;
		gz += twoKp * halfez;
	}

	// Integrate rate of change of quaternion
	gx *= (0.5f * (1.0f / sampleFreq));		// pre-multiply common factors
	gy *= (0.5f * (1.0f / sampleFreq));
	gz *= (0.5f * (1.0f / sampleFreq));
	qa = q0;
	qb = q1;
	qc = q2;
	q0 += (-qb * gx - qc * gy - q3 * gz);
	q1 += (qa * gx + qc * gz - q3 * gy);
	q2 += (qa * gy - qb * gz + q3 * gx);
	q3 += (qa * gz + qb * gy - qc * gx);

	// Normalise quaternion
	recipNorm = invSqrt(q0 * q0 + q1 * q1 + q2 * q2 + q3 * q3);
	q0 *= recipNorm;
	q1 *= recipNorm;
	q2 *= recipNorm;
	q3 *= recipNorm;


	*pitch = asin(-2 * q1 * q3 + 2 * q0* q2);	// pitch
	*roll  = atan2(2 * q2 * q3 + 2 * q0 * q1, -2 * q1 * q1 - 2 * q2* q2 + 1);	// roll
	*yaw   = atan2(2*(q1*q2 + q0*q3),q0*q0+q1*q1-q2*q2-q3*q3);	//yaw

	*pitch *= RAD_TO_DEG;
    *yaw   *= RAD_TO_DEG;
    // Declination of SparkFun Electronics (40°05'26.6"N 105°11'05.9"W) is
    // 	8° 30' E  ± 0° 21' (or 8.5°) on 2016-07-19
    // - http://www.ngdc.noaa.gov/geomag-web/#declination
    *yaw   -= 8.5;
    *roll  *= RAD_TO_DEG;

	///Serial.printf("%f    %f    %f \r\n",  pitch, roll, yaw);
}

//---------------------------------------------------------------------------------------------------
// Fast inverse square-root
// See: http://en.wikipedia.org/wiki/Fast_inverse_square_root

#pragma GCC diagnostic push
#pragma GCC diagnostic ignored "-Wstrict-aliasing"
float invSqrt(float x) {
	float halfx = 0.5f * x;
	float y = x;
	long i = *(long*)&y;
	i = 0x5f3759df - (i>>1);
	y = *(float*)&i;
	y = y * (1.5f - (halfx * y * y));
	return y;
}
#pragma GCC diagnostic pop
//====================================================================================================
// END OF CODE
//====================================================================================================
