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ACM : Attitude.pde removed stabilize D

This commit is contained in:
Jason Short 2012-11-09 21:41:50 -08:00
parent e4cec91e59
commit a42c6bb609
1 changed files with 15 additions and 15 deletions
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30
ArduCopter/Attitude.pde
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@ -305,15 +305,15 @@ get_rate_roll(int32_t target_rate)
int32_t p,i,d; // used to capture pid values for logging
int32_t current_rate; // this iteration's rate
int32_t rate_error; // simply target_rate - current_rate
int32_t rate_d; // roll's acceleration
//int32_t rate_d; // roll's acceleration
int32_t output; // output from pid controller
int32_t rate_d_dampener; // value to dampen output based on acceleration
//int32_t rate_d_dampener; // value to dampen output based on acceleration
// get current rate
current_rate = (omega.x * DEGX100);
// calculate and filter the acceleration
rate_d = roll_rate_d_filter.apply(current_rate - last_rate);
//rate_d = roll_rate_d_filter.apply(current_rate - last_rate);
// store rate for next iteration
last_rate = current_rate;
@ -333,9 +333,9 @@ get_rate_roll(int32_t target_rate)
output = p + i + d;
// Dampening output with D term
rate_d_dampener = rate_d * roll_scale_d;
rate_d_dampener = constrain(rate_d_dampener, -400, 400);
output -= rate_d_dampener;
//rate_d_dampener = rate_d * roll_scale_d;
//rate_d_dampener = constrain(rate_d_dampener, -400, 400);
//output -= rate_d_dampener;
// constrain output
output = constrain(output, -5000, 5000);
@ -348,7 +348,7 @@ get_rate_roll(int32_t target_rate)
log_counter++;
if( log_counter >= 10 ) { // (update rate / desired output rate) = (100hz / 10hz) = 10
log_counter = 0;
Log_Write_PID(CH6_RATE_KP, rate_error, p, i, d-rate_d_dampener, output, tuning_value);
Log_Write_PID(CH6_RATE_KP, rate_error, p, i, d /*-rate_d_dampener*/, output, tuning_value);
}
}
#endif
@ -364,15 +364,15 @@ get_rate_pitch(int32_t target_rate)
int32_t p,i,d; // used to capture pid values for logging
int32_t current_rate; // this iteration's rate
int32_t rate_error; // simply target_rate - current_rate
int32_t rate_d; // roll's acceleration
//int32_t rate_d; // roll's acceleration
int32_t output; // output from pid controller
int32_t rate_d_dampener; // value to dampen output based on acceleration
//int32_t rate_d_dampener; // value to dampen output based on acceleration
// get current rate
current_rate = (omega.y * DEGX100);
// calculate and filter the acceleration
rate_d = pitch_rate_d_filter.apply(current_rate - last_rate);
//rate_d = pitch_rate_d_filter.apply(current_rate - last_rate);
// store rate for next iteration
last_rate = current_rate;
@ -390,9 +390,9 @@ get_rate_pitch(int32_t target_rate)
output = p + i + d;
// Dampening output with D term
rate_d_dampener = rate_d * pitch_scale_d;
rate_d_dampener = constrain(rate_d_dampener, -400, 400);
output -= rate_d_dampener;
//rate_d_dampener = rate_d * pitch_scale_d;
//rate_d_dampener = constrain(rate_d_dampener, -400, 400);
//output -= rate_d_dampener;
// constrain output
output = constrain(output, -5000, 5000);
@ -404,7 +404,7 @@ get_rate_pitch(int32_t target_rate)
log_counter++;
if( log_counter >= 10 ) { // (update rate / desired output rate) = (100hz / 10hz) = 10
log_counter = 0;
Log_Write_PID(CH6_RATE_KP+100, rate_error, p, i, d-rate_d_dampener, output, tuning_value);
Log_Write_PID(CH6_RATE_KP+100, rate_error, p, i, d/*-rate_d_dampener*/, output, tuning_value);
}
}
#endif
@ -465,7 +465,7 @@ static int16_t
get_throttle_rate(int16_t z_target_speed)
{
int32_t p,i,d; // used to capture pid values for logging
int16_t z_rate_error, output;
int16_t z_rate_error, output = 0;
// calculate rate error
#if INERTIAL_NAV == ENABLED