Merged beta into mavlink rework branch

This commit is contained in:
Lorenz Meier
2014-01-28 15:13:14 +01:00
parent ac77fe9c27
commit 9c355d280e
220 changed files with 10717 additions and 9729 deletions
+10 -8
View File
@@ -555,6 +555,7 @@ MavlinkReceiver::handle_message(mavlink_message_t *msg)
hil_gps.alt = gps.alt;
hil_gps.eph_m = (float)gps.eph * 1e-2f; // from cm to m
hil_gps.epv_m = (float)gps.epv * 1e-2f; // from cm to m
hil_gps.timestamp_variance = gps.time_usec;
hil_gps.s_variance_m_s = 5.0f;
hil_gps.p_variance_m = hil_gps.eph_m * hil_gps.eph_m;
hil_gps.vel_m_s = (float)gps.vel * 1e-2f; // from cm/s to m/s
@@ -566,6 +567,7 @@ MavlinkReceiver::handle_message(mavlink_message_t *msg)
if (heading_rad > M_PI_F)
heading_rad -= 2.0f * M_PI_F;
hil_gps.timestamp_velocity = gps.time_usec;
hil_gps.vel_n_m_s = gps.vn * 1e-2f; // from cm to m
hil_gps.vel_e_m_s = gps.ve * 1e-2f; // from cm to m
hil_gps.vel_d_m_s = gps.vd * 1e-2f; // from cm to m
@@ -613,9 +615,9 @@ MavlinkReceiver::handle_message(mavlink_message_t *msg)
hil_global_pos.lat = hil_state.lat;
hil_global_pos.lon = hil_state.lon;
hil_global_pos.alt = hil_state.alt / 1000.0f;
hil_global_pos.vx = hil_state.vx / 100.0f;
hil_global_pos.vy = hil_state.vy / 100.0f;
hil_global_pos.vz = hil_state.vz / 100.0f;
hil_global_pos.vel_n = hil_state.vx / 100.0f;
hil_global_pos.vel_e = hil_state.vy / 100.0f;
hil_global_pos.vel_d = hil_state.vz / 100.0f;
} else {
pub_hil_global_pos = orb_advertise(ORB_ID(vehicle_global_position), &hil_global_pos);
@@ -659,8 +661,8 @@ MavlinkReceiver::handle_message(mavlink_message_t *msg)
/* Calculate Rotation Matrix */
math::Quaternion q(hil_state.attitude_quaternion);
math::Dcm C_nb(q);
math::EulerAngles euler(C_nb);
math::Matrix<3,3> C_nb = q.to_dcm();
math::Vector<3> euler = C_nb.to_euler();
/* set rotation matrix */
for (int i = 0; i < 3; i++) for (int j = 0; j < 3; j++)
@@ -675,9 +677,9 @@ MavlinkReceiver::handle_message(mavlink_message_t *msg)
hil_attitude.q[3] = q(3);
hil_attitude.q_valid = true;
hil_attitude.roll = euler.getPhi();
hil_attitude.pitch = euler.getTheta();
hil_attitude.yaw = euler.getPsi();
hil_attitude.roll = euler(0);
hil_attitude.pitch = euler(1);
hil_attitude.yaw = euler(2);
hil_attitude.rollspeed = hil_state.rollspeed;
hil_attitude.pitchspeed = hil_state.pitchspeed;
hil_attitude.yawspeed = hil_state.yawspeed;