diff options
3 files changed, 11 insertions, 3 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 5d768b73d..a835599e7 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 @@ -743,8 +743,8 @@ FixedwingEstimator::task_main() /* sets also parameters in the EKF object */ parameters_update(); - Vector3f lastAngRate = {0.0f, 0.0f, 0.0f}; - Vector3f lastAccel = {0.0f, 0.0f, 0.0f}; + Vector3f lastAngRate; + Vector3f lastAccel; /* wakeup source(s) */ struct pollfd fds[2]; diff --git a/src/modules/ekf_att_pos_estimator/estimator_23states.cpp b/src/modules/ekf_att_pos_estimator/estimator_23states.cpp index 3da92b264..a41b58250 100644 --- a/src/modules/ekf_att_pos_estimator/estimator_23states.cpp +++ b/src/modules/ekf_att_pos_estimator/estimator_23states.cpp @@ -73,7 +73,7 @@ void AttPosEKF::UpdateStrapdownEquationsNED() float qUpdated[4]; float quatMag; float deltaQuat[4]; - const Vector3f gravityNED = {0.0,0.0,GRAVITY_MSS}; + const Vector3f gravityNED(0.0f, 0.0f, GRAVITY_MSS); // Remove sensor bias errors correctedDelAng.x = dAngIMU.x - states[10]; diff --git a/src/modules/ekf_att_pos_estimator/estimator_utilities.h b/src/modules/ekf_att_pos_estimator/estimator_utilities.h index 5648cb05c..0cafdc808 100644 --- a/src/modules/ekf_att_pos_estimator/estimator_utilities.h +++ b/src/modules/ekf_att_pos_estimator/estimator_utilities.h @@ -19,6 +19,14 @@ public: float y; float z; + Vector3f() { zero(); } + + Vector3f(float a, float b, float c) : + x(a), + y(b), + z(c) + {} + float length(void) const; void zero(void); }; |