void  imu_AHRSupdate(float gx, float gy, float gz, float ax, float ay, float az, float mx, float my, float mz) { //gx,gy,gz - угловые ускорения, рад/сек
  float recipNorm;                                                                                                                                          //ax,ay,az - линейные ускорения
  float q0q0, q0q1, q0q2, q0q3, q1q1, q1q2, q1q3, q2q2, q2q3, q3q3;
  float halfex = 0.0f;
  float halfey = 0.0f;
  float halfez = 0.0f;
  float qa, qb, qc;

  // 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;

  // Use magnetometer measurement only when valid (avoids NaN in magnetometer normalisation)
  if((mx != 0.0f) && (my != 0.0f) && (mz != 0.0f)) {                                                          //Магнитомер не интересует
    float hx, hy, bx, bz;
    float halfwx, halfwy, halfwz;

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

    // 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 magnetic field
    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 = (my * halfwz - mz * halfwy);
    halfey = (mz * halfwx - mx * halfwz);
    halfez = (mx * halfwy - my * halfwx);
  }

  // Compute feedback only if accelerometer measurement valid (avoids NaN in accelerometer normalisation)
  if((ax != 0.0f) && (ay != 0.0f) && (az != 0.0f)) {
    float halfvx, halfvy, halfvz;

    // Normalise accelerometer measurement                     Нормируем вектор ускорения
    recipNorm = imu_invSqrt(ax * ax + ay * ay + az * az);
    ax *= recipNorm;
    ay *= recipNorm;
    az *= recipNorm;

    // Estimated direction of gravity  //через направляющие косинусы вычисляем вектор гравитации
    halfvx = q1q3 - q0q2;
    halfvy = q0q1 + q2q3;
    halfvz = q0q0 - 0.5f + q3q3;

    // Error is sum of cross product between estimated direction and measured direction of field vectors
    halfex += (ay * halfvz - az * halfvy);     //Непонятно зачем комбинируем вектор гравитации и измеренные ускорения!!!!
    halfey += (az * halfvx - ax * halfvz);
    halfez += (ax * halfvy - ay * halfvx);
  }

  // Apply feedback only when valid data has been gathered from the accelerometer or magnetometer
  if(halfex != 0.0f && halfey != 0.0f && halfez != 0.0f) {                        
    // 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);  //Интегрируем по времени и добавляем к угловым ускорениям - зачем!!!!!!
      integralFBz += twoKi * halfez * (1.0f / sampleFreq);  //Самое непонятное это!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!
      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  //Корректируем матрицу направляющих косинусов
  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 = imu_invSqrt(q0 * q0 + q1 * q1 + q2 * q2 + q3 * q3);
  q0 *= recipNorm;
  q1 *= recipNorm;
  q2 *= recipNorm;
  q3 *= recipNorm;
}

    halfex += (ay * halfvz - az * halfvy);     //Непонятно зачем комбинируем вектор гравитации и измеренные ускорения!!!!
    halfey += (az * halfvx - ax * halfvz);
    halfez += (ax * halfvy - ay * halfvx);
  }

  // Apply feedback only when valid data has been gathered from the accelerometer or magnetometer
  if(halfex != 0.0f && halfey != 0.0f && halfez != 0.0f) {                        
    // 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);  //Интегрируем по времени и добавляем к угловым ускорениям - зачем!!!!!!
      integralFBz += twoKi * halfez * (1.0f / sampleFreq);  //Самое непонятное это!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!
      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;
  }

if((ax != 0.0f) && (ay != 0.0f) && (az != 0.0f)) {
    float halfvx, halfvy, halfvz;

    // Normalise accelerometer measurement                     Нормируем вектор ускорения
    recipNorm = imu_invSqrt(ax * ax + ay * ay + az * az)