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ArduCopter: updated accel based throttle to use ahrs's get_accel_ef method

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Also removed slow low pass filter meant to correct for accelerometer calibration.  This is no longer required now that we have the improved calibration method.
This commit is contained in:
rmackay9 2012-12-12 16:29:46 +09:00
parent 50bd21d548
commit ff9902c5d6
1 changed files with 3 additions and 8 deletions
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11
ArduCopter/Attitude.pde
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@ -803,21 +803,16 @@ void throttle_accel_deactivate()
static int16_t
get_throttle_accel(int16_t z_target_accel)
{
static float accel_one_g = -980; // filtered estimate of 1G in cm/s/s
int32_t p,i,d; // used to capture pid values for logging
int16_t z_accel_error, output;
float z_accel_meas_temp;
Vector3f accel = ins.get_accel();
Matrix3f dcm_matrix = ahrs.get_dcm_matrix();
//Matrix3f dcm_matrix = ahrs.get_dcm_matrix();
// Calculate Earth Frame Z acceleration
z_accel_meas_temp = (dcm_matrix.c.x * accel.x + dcm_matrix.c.y * accel.y + dcm_matrix.c.z * accel.z)* 100.0;
// Filter Earth Frame Z acceleration with fc = 0.01 Hz to find 1 g
accel_one_g = accel_one_g + 0.00062792 * (z_accel_meas_temp - accel_one_g);
z_accel_meas_temp = z_accel_meas_temp - accel_one_g;
//z_accel_meas_temp = (dcm_matrix.c.x * accel.x + dcm_matrix.c.y * accel.y + dcm_matrix.c.z * accel.z)* 100.0;
z_accel_meas_temp = ahrs.get_accel_ef().z;
// Filter Earth Frame Z acceleration with fc = 1 Hz
z_accel_meas = z_accel_meas + 0.059117 * (z_accel_meas_temp - z_accel_meas);