tecs_update_pitch_throttle(alt_sp,
						   calculate_target_airspeed(mission_airspeed),
						   radians(_parameters.pitch_limit_min) - _parameters.pitchsp_offset_rad,
						   radians(_parameters.pitch_limit_max) - _parameters.pitchsp_offset_rad,
						   _parameters.throttle_min,
						   _parameters.throttle_max,
						   _parameters.throttle_cruise,
						   false,
						   radians(_parameters.pitch_limit_min));