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| author | Julian Oes <joes@student.ethz.ch> | 2013-03-13 10:53:20 -0700 |
|---|---|---|
| committer | Julian Oes <julian@oes.ch> | 2013-06-15 20:06:13 +0200 |
| commit | 8559315f4f8b6515f2ba9ceadf2aa3b73af41bdc (patch) | |
| tree | 7858cc452962a0bc98746820df516f0af8b23658 /src/modules/multirotor_att_control | |
| parent | 2b9fa731efd08a01effd87a636ae8e53994944f7 (diff) | |
| download | px4-firmware-8559315f4f8b6515f2ba9ceadf2aa3b73af41bdc.tar.gz px4-firmware-8559315f4f8b6515f2ba9ceadf2aa3b73af41bdc.tar.bz2 px4-firmware-8559315f4f8b6515f2ba9ceadf2aa3b73af41bdc.zip | |
Added a filter parameter to the pid function
Conflicts:
apps/multirotor_pos_control/multirotor_pos_control.c
Diffstat (limited to 'src/modules/multirotor_att_control')
| -rw-r--r-- | src/modules/multirotor_att_control/multirotor_attitude_control.c | 8 | ||||
| -rw-r--r-- | src/modules/multirotor_att_control/multirotor_rate_control.c | 8 |
2 files changed, 8 insertions, 8 deletions
diff --git a/src/modules/multirotor_att_control/multirotor_attitude_control.c b/src/modules/multirotor_att_control/multirotor_attitude_control.c index 1053ac7a3..d7e1a3adc 100644 --- a/src/modules/multirotor_att_control/multirotor_attitude_control.c +++ b/src/modules/multirotor_att_control/multirotor_attitude_control.c @@ -155,8 +155,8 @@ void multirotor_control_attitude(const struct vehicle_attitude_setpoint_s *att_s parameters_init(&h); parameters_update(&h, &p); - pid_init(&pitch_controller, p.att_p, p.att_i, p.att_d, 1000.0f, 1000.0f, PID_MODE_DERIVATIV_SET); - pid_init(&roll_controller, p.att_p, p.att_i, p.att_d, 1000.0f, 1000.0f, PID_MODE_DERIVATIV_SET); + pid_init(&pitch_controller, p.att_p, p.att_i, p.att_d, 1000.0f, 1000.0f, 0.0f, PID_MODE_DERIVATIV_SET); + pid_init(&roll_controller, p.att_p, p.att_i, p.att_d, 1000.0f, 1000.0f, 0.0f, PID_MODE_DERIVATIV_SET); initialized = true; } @@ -167,8 +167,8 @@ void multirotor_control_attitude(const struct vehicle_attitude_setpoint_s *att_s parameters_update(&h, &p); /* apply parameters */ - pid_set_parameters(&pitch_controller, p.att_p, p.att_i, p.att_d, 1000.0f, 1000.0f); - pid_set_parameters(&roll_controller, p.att_p, p.att_i, p.att_d, 1000.0f, 1000.0f); + pid_set_parameters(&pitch_controller, p.att_p, p.att_i, p.att_d, 1000.0f, 1000.0f, 0.0f); + pid_set_parameters(&roll_controller, p.att_p, p.att_i, p.att_d, 1000.0f, 1000.0f, 0.0f); } /* reset integral if on ground */ diff --git a/src/modules/multirotor_att_control/multirotor_rate_control.c b/src/modules/multirotor_att_control/multirotor_rate_control.c index 4ab92b955..57aea726a 100644 --- a/src/modules/multirotor_att_control/multirotor_rate_control.c +++ b/src/modules/multirotor_att_control/multirotor_rate_control.c @@ -182,17 +182,17 @@ void multirotor_control_rates(const struct vehicle_rates_setpoint_s *rate_sp, initialized = true; pid_init(&pitch_rate_controller, p.attrate_p, p.attrate_i, p.attrate_d, 1000.0f, - 1000.0f, PID_MODE_DERIVATIV_CALC); + 1000.0f, 0.2f, PID_MODE_DERIVATIV_CALC); pid_init(&roll_rate_controller, p.attrate_p, p.attrate_i, p.attrate_d, 1000.0f, - 1000.0f, PID_MODE_DERIVATIV_CALC); + 1000.0f, 0.2f, PID_MODE_DERIVATIV_CALC); } /* load new parameters with lower rate */ if (motor_skip_counter % 2500 == 0) { /* update parameters from storage */ parameters_update(&h, &p); - pid_set_parameters(&pitch_rate_controller, p.attrate_p, p.attrate_i, p.attrate_d, 1000.0f, 1000.0f); - pid_set_parameters(&roll_rate_controller, p.attrate_p, p.attrate_i, p.attrate_d, 1000.0f, 1000.0f); + pid_set_parameters(&pitch_rate_controller, p.attrate_p, p.attrate_i, p.attrate_d, 1000.0f, 1000.0f, 0.2f); + pid_set_parameters(&roll_rate_controller, p.attrate_p, p.attrate_i, p.attrate_d, 1000.0f, 1000.0f, 0.2f); } /* control pitch (forward) output */ |