diff options
Diffstat (limited to 'src/lib/ecl/attitude_fw/ecl_roll_controller.cpp')
| -rw-r--r-- | src/lib/ecl/attitude_fw/ecl_roll_controller.cpp | 7 |
1 files changed, 2 insertions, 5 deletions
diff --git a/src/lib/ecl/attitude_fw/ecl_roll_controller.cpp b/src/lib/ecl/attitude_fw/ecl_roll_controller.cpp index 82903ef5a..9894a34d7 100644 --- a/src/lib/ecl/attitude_fw/ecl_roll_controller.cpp +++ b/src/lib/ecl/attitude_fw/ecl_roll_controller.cpp @@ -59,9 +59,9 @@ ECL_RollController::ECL_RollController() : _integrator(0.0f), _rate_error(0.0f), _rate_setpoint(0.0f), - _bodyrate_setpoint(0.0f) + _bodyrate_setpoint(0.0f), + _nonfinite_input_perf(perf_alloc(PC_COUNT, "fw att control roll nonfinite input")) { - perf_alloc(PC_COUNT, "fw att control roll nonfinite input"); } ECL_RollController::~ECL_RollController() @@ -114,9 +114,6 @@ float ECL_RollController::control_bodyrate(float pitch, if (dt_micros > 500000) lock_integrator = true; -// float k_ff = math::max((_k_p - _k_i * _tc) * _tc - _k_d, 0.0f); - float k_ff = 0; //xxx: param - /* input conditioning */ // warnx("airspeed pre %.4f", (double)airspeed); if (!isfinite(airspeed)) { |