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Diffstat (limited to 'src/modules/ekf_att_pos_estimator/ekf_att_pos_estimator_main.cpp')
-rw-r--r--src/modules/ekf_att_pos_estimator/ekf_att_pos_estimator_main.cpp22
1 files changed, 2 insertions, 20 deletions
diff --git a/src/modules/ekf_att_pos_estimator/ekf_att_pos_estimator_main.cpp b/src/modules/ekf_att_pos_estimator/ekf_att_pos_estimator_main.cpp
index c384b2566..b7e118d47 100644
--- a/src/modules/ekf_att_pos_estimator/ekf_att_pos_estimator_main.cpp
+++ b/src/modules/ekf_att_pos_estimator/ekf_att_pos_estimator_main.cpp
@@ -1220,30 +1220,12 @@ FixedwingEstimator::task_main()
} else if (_ekf->statesInitialised) {
// We're apparently initialized in this case now
- int check = check_filter_state();
-
- if (check) {
- // Let the system re-initialize itself
- continue;
- }
+ // check (and reset the filter as needed)
+ (void)check_filter_state();
// Run the strapdown INS equations every IMU update
_ekf->UpdateStrapdownEquationsNED();
- #if 0
- // debug code - could be tunred into a filter mnitoring/watchdog function
- float tempQuat[4];
-
- for (uint8_t j = 0; j <= 3; j++) tempQuat[j] = states[j];
-
- quat2eul(eulerEst, tempQuat);
- for (uint8_t j = 0; j <= 2; j++) eulerDif[j] = eulerEst[j] - ahrsEul[j];
-
- if (eulerDif[2] > pi) eulerDif[2] -= 2 * pi;
-
- if (eulerDif[2] < -pi) eulerDif[2] += 2 * pi;
-
- #endif
// store the predicted states for subsequent use by measurement fusion
_ekf->StoreStates(IMUmsec);
// Check if on ground - status is used by covariance prediction