aboutsummaryrefslogtreecommitdiff
path: root/src
diff options
context:
space:
mode:
authorLorenz Meier <lm@inf.ethz.ch>2013-09-01 05:13:14 -0700
committerLorenz Meier <lm@inf.ethz.ch>2013-09-01 05:13:14 -0700
commita660dc3fa6dd8c4bee54b834cec6ce1a94a44b33 (patch)
treef763e14557b8c75a5683c9c8501b0364a989eef6 /src
parent806fb0b076850741174b338c4a93798da708daba (diff)
parent6a6fe6937146723cb86dc0fc6e46db38b328dacd (diff)
downloadpx4-firmware-a660dc3fa6dd8c4bee54b834cec6ce1a94a44b33.tar.gz
px4-firmware-a660dc3fa6dd8c4bee54b834cec6ce1a94a44b33.tar.bz2
px4-firmware-a660dc3fa6dd8c4bee54b834cec6ce1a94a44b33.zip
Merge pull request #367 from limhyon/master
Bug resolved & new data for setpoint topic.
Diffstat (limited to 'src')
-rwxr-xr-xsrc/modules/attitude_estimator_so3_comp/attitude_estimator_so3_comp_main.cpp4
-rwxr-xr-xsrc/modules/position_estimator_mc/position_estimator_mc_main.c7
-rw-r--r--src/modules/uORB/topics/vehicle_attitude_setpoint.h6
3 files changed, 14 insertions, 3 deletions
diff --git a/src/modules/attitude_estimator_so3_comp/attitude_estimator_so3_comp_main.cpp b/src/modules/attitude_estimator_so3_comp/attitude_estimator_so3_comp_main.cpp
index 236052b56..86bda3c75 100755
--- a/src/modules/attitude_estimator_so3_comp/attitude_estimator_so3_comp_main.cpp
+++ b/src/modules/attitude_estimator_so3_comp/attitude_estimator_so3_comp_main.cpp
@@ -730,7 +730,7 @@ const unsigned int loop_interval_alarm = 6500; // loop interval in microseconds
// Because proper mount of PX4 will give you a reversed accelerometer readings.
NonlinearSO3AHRSupdate(gyro[0],gyro[1],gyro[2],-acc[0],-acc[1],-acc[2],mag[0],mag[1],mag[2],so3_comp_params.Kp,so3_comp_params.Ki, dt);
- // Convert q->R.
+ // Convert q->R, This R converts inertial frame to body frame.
Rot_matrix[0] = q0q0 + q1q1 - q2q2 - q3q3;// 11
Rot_matrix[1] = 2.0 * (q1*q2 + q0*q3); // 12
Rot_matrix[2] = 2.0 * (q1*q3 - q0*q2); // 13
@@ -794,7 +794,7 @@ const unsigned int loop_interval_alarm = 6500; // loop interval in microseconds
memcpy(&att.rate_offsets, &(gyro_bias), sizeof(att.rate_offsets));
/* copy rotation matrix */
- memcpy(&att.R, Rot_matrix, sizeof(Rot_matrix));
+ memcpy(&att.R, Rot_matrix, sizeof(float)*9);
att.R_valid = true;
if (isfinite(att.roll) && isfinite(att.pitch) && isfinite(att.yaw)) {
diff --git a/src/modules/position_estimator_mc/position_estimator_mc_main.c b/src/modules/position_estimator_mc/position_estimator_mc_main.c
index 984bd1329..363961819 100755
--- a/src/modules/position_estimator_mc/position_estimator_mc_main.c
+++ b/src/modules/position_estimator_mc/position_estimator_mc_main.c
@@ -497,7 +497,12 @@ int position_estimator_mc_thread_main(int argc, char *argv[])
local_pos_est.vz = x_z_aposteriori_k[1];
local_pos_est.timestamp = hrt_absolute_time();
if ((isfinite(x_x_aposteriori_k[0])) && (isfinite(x_x_aposteriori_k[1])) && (isfinite(x_y_aposteriori_k[0])) && (isfinite(x_y_aposteriori_k[1])) && (isfinite(x_z_aposteriori_k[0])) && (isfinite(x_z_aposteriori_k[1]))){
- orb_publish(ORB_ID(vehicle_local_position), local_pos_est_pub, &local_pos_est);
+ if(local_pos_est_pub > 0)
+ orb_publish(ORB_ID(vehicle_local_position), local_pos_est_pub, &local_pos_est);
+ else
+ local_pos_est_pub = orb_advertise(ORB_ID(vehicle_local_position), &local_pos_est);
+ //char buf[0xff]; sprintf(buf,"[pos_est_mc] x:%f, y:%f, z:%f",x_x_aposteriori_k[0],x_y_aposteriori_k[0],x_z_aposteriori_k[0]);
+ //mavlink_log_info(mavlink_fd, buf);
}
}
} /* end of poll return value check */
diff --git a/src/modules/uORB/topics/vehicle_attitude_setpoint.h b/src/modules/uORB/topics/vehicle_attitude_setpoint.h
index a7cda34a8..686fd765c 100644
--- a/src/modules/uORB/topics/vehicle_attitude_setpoint.h
+++ b/src/modules/uORB/topics/vehicle_attitude_setpoint.h
@@ -64,6 +64,12 @@ struct vehicle_attitude_setpoint_s
float R_body[9]; /**< Rotation matrix describing the setpoint as rotation from the current body frame */
bool R_valid; /**< Set to true if rotation matrix is valid */
+ //! For quaternion-based attitude control
+ float q_d[4]; /** Desired quaternion for quaternion control */
+ bool q_d_valid; /**< Set to true if quaternion vector is valid */
+ float q_e[4]; /** Attitude error in quaternion */
+ bool q_e_valid; /**< Set to true if quaternion error vector is valid */
+
float thrust; /**< Thrust in Newton the power system should generate */
};