diff options
Diffstat (limited to 'src/lib/ecl/attitude_fw/ecl_pitch_controller.cpp')
| -rw-r--r-- | src/lib/ecl/attitude_fw/ecl_pitch_controller.cpp | 6 |
1 files changed, 3 insertions, 3 deletions
diff --git a/src/lib/ecl/attitude_fw/ecl_pitch_controller.cpp b/src/lib/ecl/attitude_fw/ecl_pitch_controller.cpp index b840206d5..8ee8b9c68 100644 --- a/src/lib/ecl/attitude_fw/ecl_pitch_controller.cpp +++ b/src/lib/ecl/attitude_fw/ecl_pitch_controller.cpp @@ -69,13 +69,13 @@ ECL_PitchController::ECL_PitchController() : _rate_error(0.0f), _rate_setpoint(0.0f), _bodyrate_setpoint(0.0f) - //_nonfinite_input_perf(perf_alloc(PC_COUNT, "fw att control pitch nonfinite input")) + _nonfinite_input_perf(perf_alloc(PC_COUNT, "fw att control pitch nonfinite input")) { } ECL_PitchController::~ECL_PitchController() { - //perf_free(_nonfinite_input_perf); + perf_free(_nonfinite_input_perf); } float ECL_PitchController::control_attitude(float pitch_setpoint, float roll, float pitch, float airspeed) @@ -145,7 +145,7 @@ float ECL_PitchController::control_bodyrate(float roll, float pitch, if (!(isfinite(roll) && isfinite(pitch) && isfinite(pitch_rate) && isfinite(yaw_rate) && isfinite(yaw_rate_setpoint) && isfinite(airspeed_min) && isfinite(airspeed_max) && isfinite(scaler))) { - //perf_count(_nonfinite_input_perf); + perf_count(_nonfinite_input_perf); return math::constrain(_last_output, -1.0f, 1.0f); } |