diff options
Diffstat (limited to 'src/modules/attitude_estimator_ekf')
| -rwxr-xr-x | src/modules/attitude_estimator_ekf/attitude_estimator_ekf_main.cpp | 4 |
1 files changed, 2 insertions, 2 deletions
diff --git a/src/modules/attitude_estimator_ekf/attitude_estimator_ekf_main.cpp b/src/modules/attitude_estimator_ekf/attitude_estimator_ekf_main.cpp index 6068ab082..4c64c88ae 100755 --- a/src/modules/attitude_estimator_ekf/attitude_estimator_ekf_main.cpp +++ b/src/modules/attitude_estimator_ekf/attitude_estimator_ekf_main.cpp @@ -568,7 +568,7 @@ const unsigned int loop_interval_alarm = 6500; // loop interval in microseconds R = R_decl * R_body; /* copy rotation matrix */ - memcpy(&att.R[0][0], &R.data[0][0], sizeof(att.R)); + memcpy(&att.R[0], &R.data[0][0], sizeof(att.R)); att.R_valid = true; // compute secondary attitude @@ -595,7 +595,7 @@ const unsigned int loop_interval_alarm = 6500; // loop interval in microseconds att.pitch_sec = euler_angles_sec(1); att.yaw_sec = euler_angles_sec(2); - memcpy(&att.R_sec[0][0], &R_adapted.data[0][0], sizeof(att.R_sec)); + memcpy(&att.R_sec[0], &R_adapted.data[0], sizeof(att.R_sec)); att.rollspeed_sec = -x_aposteriori[2]; att.pitchspeed_sec = x_aposteriori[1]; |