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px4-firmware
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Fix a number of interface scaling / offset stupidities, should be closer to operational now on HW.

This commit is contained in:
Lorenz Meier 2014-01-31 14:08:27 +01:00
parent 9695ae8cee
commit d4ccd9bc45
1 changed files with 39 additions and 30 deletions
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69
src/modules/fw_att_pos_estimator/fw_att_pos_estimator_main.cpp
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@ -596,7 +596,7 @@ FixedwingEstimator::task_main()
gpsGndSpd = sqrtf(_gps.vel_n_m_s * _gps.vel_n_m_s + _gps.vel_e_m_s * _gps.vel_e_m_s);
gpsVelD = _gps.vel_d_m_s;
gpsLat = math::radians(_gps.lat / (double)1e7);
gpsLon = math::radians(_gps.lon / (double)1e7);
gpsLon = math::radians(_gps.lon / (double)1e7) - M_PI;
gpsHgt = _gps.alt / 1e3f;
if (hrt_elapsed_time(&start_time) > 500000 && !_initialized) {
@ -610,7 +610,9 @@ FixedwingEstimator::task_main()
if (_initialized) {
/* convert GPS measurements to horizontal NE, altitude and 3D velocity NED */
calcvelNED(velNED, gpsCourse, gpsGndSpd, gpsVelD);
velNED[0] = _gps.vel_n_m_s;
velNED[1] = _gps.vel_e_m_s;
velNED[2] = _gps.vel_d_m_s;
calcposNED(posNED, gpsLat, gpsLon, gpsHgt, latRef, lonRef, hgtRef);
posNE[0] = posNED[0];
@ -657,30 +659,28 @@ FixedwingEstimator::task_main()
orb_copy(ORB_ID(sensor_mag), _mag_sub, &_mag);
// XXX we compensate the offsets upfront - should be close to zero.
// XXX the purpose of the 0.001 factor is unclear
// 0.001f
magData.x = 0.001f * _mag.x;
magBias.x = 0.0f; // _mag_offsets.x_offset
magData.x = _mag.x;
magBias.x = 0.0001f; // _mag_offsets.x_offset
magData.y = 0.001f * _mag.y;
magBias.y = 0.0f; // _mag_offsets.y_offset
magData.y = _mag.y;
magBias.y = 0.0001f; // _mag_offsets.y_offset
magData.z = 0.001f * _mag.z;
magBias.z = 0.0f; // _mag_offsets.y_offset
magData.z = _mag.z;
magBias.z = 0.0001f; // _mag_offsets.y_offset
#else
// XXX we compensate the offsets upfront - should be close to zero.
// XXX the purpose of the 0.001 factor is unclear
// 0.001f
magData.x = 0.001f * _sensor_combined.magnetometer_ga[0];
magBias.x = 0.0f; // _mag_offsets.x_offset
magData.x = _sensor_combined.magnetometer_ga[0];
magBias.x = 0.0001f; // _mag_offsets.x_offset
magData.y = 0.001f * _sensor_combined.magnetometer_ga[1];
magBias.y = 0.0f; // _mag_offsets.y_offset
magData.y = _sensor_combined.magnetometer_ga[1];
magBias.y = 0.0001f; // _mag_offsets.y_offset
magData.z = 0.001f * _sensor_combined.magnetometer_ga[2];
magBias.z = 0.0f; // _mag_offsets.y_offset
magData.z = _sensor_combined.magnetometer_ga[2];
magBias.z = 0.0001f; // _mag_offsets.y_offset
#endif
@ -749,14 +749,14 @@ FixedwingEstimator::task_main()
_att.roll = euler.getPhi();
_att.pitch = euler.getTheta();
_att.yaw = euler.getPsi();
// XXX find the right state
_att.rollspeed = _gyro.x - states[11];
_att.pitchspeed = _gyro.y - states[12];
_att.yawspeed = _gyro.z - states[13];
_att.rollspeed = angRate.x - states[10];
_att.pitchspeed = angRate.y - states[11];
_att.yawspeed = angRate.z - states[12];
// gyro offsets
_att.rate_offsets[0] = states[11];
_att.rate_offsets[1] = states[12];
_att.rate_offsets[2] = states[13];
_att.rate_offsets[0] = states[10];
_att.rate_offsets[1] = states[11];
_att.rate_offsets[2] = states[12];
/* lazily publish the attitude only once available */
if (_att_pub > 0) {
@ -880,13 +880,22 @@ int fw_att_pos_estimator_main(int argc, char *argv[])
printf("attitude: roll: %8.4f, pitch %8.4f, yaw: %8.4f degrees\n",
(double)math::degrees(euler.getPhi()), (double)math::degrees(euler.getTheta()), (double)math::degrees(euler.getPsi()));
printf("states (quat) [1-4]: %8.4f, %8.4f, %8.4f, %8.4f\n", (double)states[0], (double)states[1], (double)states[2], (double)states[3]);
printf("states (vel) [5-7]: %8.4f, %8.4f, %8.4f\n", (double)states[4], (double)states[5], (double)states[6]);
printf("states (pos) [8-10]: %8.4f, %8.4f, %8.4f\n", (double)states[7], (double)states[8], (double)states[9]);
printf("states [11-13]: %8.4f, %8.4f, %8.4f\n", (double)states[10], (double)states[11], (double)states[12]);
printf("states [14-16]: %8.4f, %8.4f, %8.4f\n", (double)states[13], (double)states[14], (double)states[15]);
printf("states [17-19]: %8.4f, %8.4f, %8.4f\n", (double)states[16], (double)states[17], (double)states[18]);
printf("states [20-21]: %8.4f, %8.4f\n", (double)states[19], (double)states[20]);
// State vector:
// 0-3: quaternions (q0, q1, q2, q3)
// 4-6: Velocity - m/sec (North, East, Down)
// 7-9: Position - m (North, East, Down)
// 10-12: Delta Angle bias - rad (X,Y,Z)
// 13-14: Wind Vector - m/sec (North,East)
// 15-17: Earth Magnetic Field Vector - milligauss (North, East, Down)
// 18-20: Body Magnetic Field Vector - milligauss (X,Y,Z)
printf("states (quat) [1-4]: %8.4f, %8.4f, %8.4f, %8.4f\n", (double)states[0], (double)states[1], (double)states[2], (double)states[3]);
printf("states (vel m/s) [5-7]: %8.4f, %8.4f, %8.4f\n", (double)states[4], (double)states[5], (double)states[6]);
printf("states (pos m) [8-10]: %8.4f, %8.4f, %8.4f\n", (double)states[7], (double)states[8], (double)states[9]);
printf("states (delta ang) [11-13]: %8.4f, %8.4f, %8.4f\n", (double)states[10], (double)states[11], (double)states[12]);
printf("states (wind) [14-15]: %8.4f, %8.4f\n", (double)states[13], (double)states[14]);
printf("states (earth mag) [16-18]: %8.4f, %8.4f, %8.4f\n", (double)states[15], (double)states[16], (double)states[17]);
printf("states (body mag) [19-21]: %8.4f, %8.4f, %8.4f\n", (double)states[18], (double)states[19], (double)states[20]);
exit(0);
} else {