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authorLorenz Meier <lm@inf.ethz.ch>2012-10-13 12:25:30 +0200
committerLorenz Meier <lm@inf.ethz.ch>2012-10-13 12:25:30 +0200
commit4dbf7befe369ba00a73945a0193f0a061c271dc3 (patch)
tree63327c7c8984f6f0bc521525de0c410c3d9f0121
parentd62ec78ab835153ef3ba480a5a4110465ba34372 (diff)
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Disable rate control, disable offset estimation
-rw-r--r--apps/attitude_estimator_ekf/attitude_estimator_ekf_main.c7
-rw-r--r--apps/commander/state_machine_helper.c12
2 files changed, 10 insertions, 9 deletions
diff --git a/apps/attitude_estimator_ekf/attitude_estimator_ekf_main.c b/apps/attitude_estimator_ekf/attitude_estimator_ekf_main.c
index 66c58f74f..1d4df87fe 100644
--- a/apps/attitude_estimator_ekf/attitude_estimator_ekf_main.c
+++ b/apps/attitude_estimator_ekf/attitude_estimator_ekf_main.c
@@ -418,9 +418,10 @@ int attitude_estimator_ekf_thread_main(int argc, char *argv[])
att.pitch = euler[1];
att.yaw = euler[2];
- att.rollspeed = x_aposteriori[0];
- att.pitchspeed = x_aposteriori[1];
- att.yawspeed = x_aposteriori[2];
+ // XXX replace with x_apo after fix to filter
+ att.rollspeed = raw.gyro_rad_s[0]; //x_aposteriori[0];
+ att.pitchspeed = raw.gyro_rad_s[1]; //x_aposteriori[1];
+ att.yawspeed = raw.gyro_rad_s[2]; //x_aposteriori[2];
/* copy offsets */
memcpy(&att.rate_offsets, &(x_aposteriori[3]), sizeof(att.rate_offsets));
diff --git a/apps/commander/state_machine_helper.c b/apps/commander/state_machine_helper.c
index 57512bfd5..7d766bcdb 100644
--- a/apps/commander/state_machine_helper.c
+++ b/apps/commander/state_machine_helper.c
@@ -501,10 +501,10 @@ void update_state_machine_mode_manual(int status_pub, struct vehicle_status_s *c
{
int old_mode = current_status->flight_mode;
current_status->flight_mode = VEHICLE_FLIGHT_MODE_MANUAL;
- current_status->flag_control_manual_enabled = true; //XXX
+ current_status->flag_control_manual_enabled = true;
/* enable attitude control per default */
current_status->flag_control_attitude_enabled = true;
- current_status->flag_control_rates_enabled = true;
+ current_status->flag_control_rates_enabled = false; // XXX
if (old_mode != current_status->flight_mode) state_machine_publish(status_pub, current_status, mavlink_fd);
if (current_status->state_machine == SYSTEM_STATE_GROUND_READY || current_status->state_machine == SYSTEM_STATE_STABILIZED || current_status->state_machine == SYSTEM_STATE_AUTO) {
@@ -517,9 +517,9 @@ void update_state_machine_mode_stabilized(int status_pub, struct vehicle_status_
{
int old_mode = current_status->flight_mode;
current_status->flight_mode = VEHICLE_FLIGHT_MODE_STABILIZED;
- current_status->flag_control_manual_enabled = true; //XXX
+ current_status->flag_control_manual_enabled = true;
current_status->flag_control_attitude_enabled = true;
- current_status->flag_control_rates_enabled = true;
+ current_status->flag_control_rates_enabled = false; // XXX
if (old_mode != current_status->flight_mode) state_machine_publish(status_pub, current_status, mavlink_fd);
if (current_status->state_machine == SYSTEM_STATE_GROUND_READY || current_status->state_machine == SYSTEM_STATE_MANUAL || current_status->state_machine == SYSTEM_STATE_AUTO) {
@@ -532,9 +532,9 @@ void update_state_machine_mode_auto(int status_pub, struct vehicle_status_s *cur
{
int old_mode = current_status->flight_mode;
current_status->flight_mode = VEHICLE_FLIGHT_MODE_AUTO;
- current_status->flag_control_manual_enabled = true; //XXX
+ current_status->flag_control_manual_enabled = true;
current_status->flag_control_attitude_enabled = true;
- current_status->flag_control_rates_enabled = true;
+ current_status->flag_control_rates_enabled = false; // XXX
if (old_mode != current_status->flight_mode) state_machine_publish(status_pub, current_status, mavlink_fd);
if (current_status->state_machine == SYSTEM_STATE_GROUND_READY || current_status->state_machine == SYSTEM_STATE_MANUAL || current_status->state_machine == SYSTEM_STATE_STABILIZED) {