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tecs: fix typo init(i)alized

This commit is contained in:
Matthias Grob 2020-05-29 15:47:34 +02:00 committed by Roman Bapst
parent 86fc94b75a
commit d0ddda8917
2 changed files with 6 additions and 6 deletions
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8
tecs/tecs.cpp
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@ -74,7 +74,7 @@ void TECS::update_vehicle_state_estimates(float airspeed, const matrix::Dcmf &ro
} }
if (reset_altitude) { if (reset_altitude) {
_states_initalized = false; _states_initialized = false;
} }
_state_update_timestamp = now; _state_update_timestamp = now;
@ -100,7 +100,7 @@ void TECS::update_vehicle_state_estimates(float airspeed, const matrix::Dcmf &ro
} }
if (!_in_air) { if (!_in_air) {
_states_initalized = false; _states_initialized = false;
} }
} }
@ -477,7 +477,7 @@ void TECS::_update_pitch_setpoint()
void TECS::_initialize_states(float pitch, float throttle_cruise, float baro_altitude, float pitch_min_climbout, void TECS::_initialize_states(float pitch, float throttle_cruise, float baro_altitude, float pitch_min_climbout,
float EAS2TAS) float EAS2TAS)
{ {
if (_pitch_update_timestamp == 0 || _dt > DT_MAX || !_in_air || !_states_initalized) { if (_pitch_update_timestamp == 0 || _dt > DT_MAX || !_in_air || !_states_initialized) {
// On first time through or when not using TECS of if there has been a large time slip, // On first time through or when not using TECS of if there has been a large time slip,
// states must be reset to allow filters to a clean start // states must be reset to allow filters to a clean start
_vert_vel_state = 0.0f; _vert_vel_state = 0.0f;
@ -525,7 +525,7 @@ void TECS::_initialize_states(float pitch, float throttle_cruise, float baro_alt
_uncommanded_descent_recovery = false; _uncommanded_descent_recovery = false;
} }
_states_initalized = true; _states_initialized = true;
} }
void TECS::_update_STE_rate_lim() void TECS::_update_STE_rate_lim()

4
tecs/tecs.h
View File

@ -89,7 +89,7 @@ public:
float get_pitch_setpoint() { return _pitch_setpoint; } float get_pitch_setpoint() { return _pitch_setpoint; }
float get_speed_weight() { return _pitch_speed_weight; } float get_speed_weight() { return _pitch_speed_weight; }
void reset_state() { _states_initalized = false; } void reset_state() { _states_initialized = false; }
enum ECL_TECS_MODE { enum ECL_TECS_MODE {
ECL_TECS_MODE_NORMAL = 0, ECL_TECS_MODE_NORMAL = 0,
@ -270,7 +270,7 @@ private:
bool _uncommanded_descent_recovery{false}; ///< true when a continuous descent caused by an unachievable airspeed demand has been detected bool _uncommanded_descent_recovery{false}; ///< true when a continuous descent caused by an unachievable airspeed demand has been detected
bool _climbout_mode_active{false}; ///< true when in climbout mode bool _climbout_mode_active{false}; ///< true when in climbout mode
bool _airspeed_enabled{false}; ///< true when airspeed use has been enabled bool _airspeed_enabled{false}; ///< true when airspeed use has been enabled
bool _states_initalized{false}; ///< true when TECS states have been iniitalized bool _states_initialized{false}; ///< true when TECS states have been iniitalized
bool _in_air{false}; ///< true when the vehicle is flying bool _in_air{false}; ///< true when the vehicle is flying
/** /**