diff options
Diffstat (limited to 'src/modules')
-rw-r--r-- | src/modules/commander/commander.cpp | 2 | ||||
-rw-r--r-- | src/modules/ekf_att_pos_estimator/estimator_22states.cpp | 15 | ||||
-rw-r--r-- | src/modules/uORB/uORB.cpp | 4 |
3 files changed, 12 insertions, 9 deletions
diff --git a/src/modules/commander/commander.cpp b/src/modules/commander/commander.cpp index 3c71195fb..adf1b0950 100644 --- a/src/modules/commander/commander.cpp +++ b/src/modules/commander/commander.cpp @@ -1340,7 +1340,7 @@ int commander_thread_main(int argc, char *argv[]) status.vtol_fw_permanent_stab = vtol_status.fw_permanent_stab; /* Make sure that this is only adjusted if vehicle realy is of type vtol*/ - if (status.system_type == VEHICLE_TYPE_VTOL_DUOROTOR || VEHICLE_TYPE_VTOL_QUADROTOR) { + if ((status.system_type == VEHICLE_TYPE_VTOL_DUOROTOR) || (status.system_type == VEHICLE_TYPE_VTOL_QUADROTOR)) { status.is_rotary_wing = vtol_status.vtol_in_rw_mode; } } diff --git a/src/modules/ekf_att_pos_estimator/estimator_22states.cpp b/src/modules/ekf_att_pos_estimator/estimator_22states.cpp index b062097fb..6cff4b948 100644 --- a/src/modules/ekf_att_pos_estimator/estimator_22states.cpp +++ b/src/modules/ekf_att_pos_estimator/estimator_22states.cpp @@ -181,9 +181,12 @@ void AttPosEKF::UpdateStrapdownEquationsNED() correctedDelAng.x = dAngIMU.x - states[10]; correctedDelAng.y = dAngIMU.y - states[11]; correctedDelAng.z = dAngIMU.z - states[12]; - dVelIMU.x = dVelIMU.x; - dVelIMU.y = dVelIMU.y; - dVelIMU.z = dVelIMU.z - states[13]; + + Vector3f dVelIMURel; + + dVelIMURel.x = dVelIMU.x; + dVelIMURel.y = dVelIMU.y; + dVelIMURel.z = dVelIMU.z - states[13]; delAngTotal.x += correctedDelAng.x; delAngTotal.y += correctedDelAng.y; @@ -263,9 +266,9 @@ void AttPosEKF::UpdateStrapdownEquationsNED() // transform body delta velocities to delta velocities in the nav frame // * and + operators have been overloaded //delVelNav = Tbn*dVelIMU + gravityNED*dtIMU; - delVelNav.x = Tbn.x.x*dVelIMU.x + Tbn.x.y*dVelIMU.y + Tbn.x.z*dVelIMU.z + gravityNED.x*dtIMU; - delVelNav.y = Tbn.y.x*dVelIMU.x + Tbn.y.y*dVelIMU.y + Tbn.y.z*dVelIMU.z + gravityNED.y*dtIMU; - delVelNav.z = Tbn.z.x*dVelIMU.x + Tbn.z.y*dVelIMU.y + Tbn.z.z*dVelIMU.z + gravityNED.z*dtIMU; + delVelNav.x = Tbn.x.x*dVelIMURel.x + Tbn.x.y*dVelIMURel.y + Tbn.x.z*dVelIMURel.z + gravityNED.x*dtIMU; + delVelNav.y = Tbn.y.x*dVelIMURel.x + Tbn.y.y*dVelIMURel.y + Tbn.y.z*dVelIMURel.z + gravityNED.y*dtIMU; + delVelNav.z = Tbn.z.x*dVelIMURel.x + Tbn.z.y*dVelIMURel.y + Tbn.z.z*dVelIMURel.z + gravityNED.z*dtIMU; // calculate the magnitude of the nav acceleration (required for GPS // variance estimation) diff --git a/src/modules/uORB/uORB.cpp b/src/modules/uORB/uORB.cpp index 149b8f6d2..cc6617aea 100644 --- a/src/modules/uORB/uORB.cpp +++ b/src/modules/uORB/uORB.cpp @@ -1,6 +1,6 @@ /**************************************************************************** * - * Copyright (C) 2012 PX4 Development Team. All rights reserved. + * Copyright (Cc) 2012-2015 PX4 Development Team. All rights reserved. * * Redistribution and use in source and binary forms, with or without * modification, are permitted provided that the following conditions @@ -230,7 +230,7 @@ ORBDevNode::open(struct file *filp) ret = CDev::open(filp); if (ret != OK) - free(sd); + delete sd; return ret; } |