Airspeed.cpp File Reference

#include <AP_ADC/AP_ADC.h>
#include <AP_Airspeed/AP_Airspeed.h>
#include <AP_HAL/AP_HAL.h>
#include <AP_BoardConfig/AP_BoardConfig.h>
#include <GCS_MAVLink/GCS_Dummy.h>

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Classes
class	GCS_MAVLINK
	MAVLink transport control class. More...

Functions
void	setup ()
void	loop ()
	AP_HAL_MAIN ()

Variables
const AP_HAL::HAL &	hal = AP_HAL::get_HAL()
	-*- tab-width: 4; Mode: C++; c-basic-offset: 4; indent-tabs-mode: nil -*- More...
float	temperature
AP_Airspeed	airspeed
static AP_BoardConfig	board_config
GCS_Dummy	_gcs

Function Documentation

AP_HAL_MAIN()

AP_HAL_MAIN

(

)

loop()

void loop

(

void

)

Definition at line 64 of file Airspeed.cpp.

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setup()

void setup

(

void

)

Definition at line 50 of file Airspeed.cpp.

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Variable Documentation

_gcs

GCS_Dummy _gcs

Definition at line 81 of file Airspeed.cpp.

airspeed

AP_Airspeed airspeed

Definition at line 34 of file Airspeed.cpp.

Referenced by GCS_MAVLINK::_handle_command_preflight_calibration_baro(), HALSITL::SITL_State::_update_airspeed(), AP_Arming::airspeed_checks(), NavEKF2_core::detectFlight(), NavEKF3_core::detectFlight(), AP_AHRS_DCM::drift_correction(), AP_AHRS_DCM::estimate_wind(), AP_AHRS::groundspeed_vector(), AP_Airspeed::last_update_ms(), DataFlash_Class::Log_Write_Airspeed(), AP_Landing_Deepstall::override_servos(), GCS_MAVLINK::send_scaled_pressure(), AP_AHRS::set_airspeed(), AP_Airspeed::set_HIL(), AP_Airspeed::setHIL(), Airspeed_Calibration::update(), GCS_MAVLINK::vfr_hud_airspeed(), and DataFlash_Class::WritesEnabled().

board_config

AP_BoardConfig board_config

static

Definition at line 35 of file Airspeed.cpp.

hal

const AP_HAL::HAL& hal = AP_HAL::get_HAL()

-*- tab-width: 4; Mode: C++; c-basic-offset: 4; indent-tabs-mode: nil -*-

The strategy for roll/pitch autotune is to give the user a AUTOTUNE flight mode which behaves just like FBWA, but does automatic tuning.

While the user is flying in AUTOTUNE the gains are saved every 10 seconds, but the saved gains are not the current gains, instead it saves the gains from 10s ago. When the user exits AUTOTUNE the gains are restored from 10s ago.

This allows the user to fly as much as they want in AUTOTUNE mode, and if they are ever unhappy they just exit the mode. If they stay in AUTOTUNE for more than 10s then their gains will have changed.

Using this approach users don't need any special switches, they just need to be able to enter and exit AUTOTUNE mode

Definition at line 30 of file Airspeed.cpp.

temperature

float temperature

Definition at line 32 of file Airspeed.cpp.

Referenced by AP_Baro_MS56XX::_calculate_5607(), AP_Baro_MS56XX::_calculate_5611(), AP_Baro_MS56XX::_calculate_5637(), AP_Baro_MS56XX::_calculate_5837(), AP_Baro_Backend::_copy_to_frontend(), AP_Airspeed_SDP3X::_correct_pressure(), AP_InertialSensor_Backend::_publish_temperature(), AP_InertialSensor_Backend::_set_gyro_raw_sample_rate(), AP_Airspeed_SDP3X::_timer(), AP_Baro_KellerLD::_update_and_wrap_accumulator(), AP_Airspeed::get_airspeed_ratio(), AP_BattMonitor::get_temperature(), AP_BattMonitor_UAVCAN::has_current(), DataFlash_Class::Log_Write_Airspeed(), DataFlash_Class::Log_Write_Baro_instance(), DataFlash_Class::Log_Write_Current_instance(), DataFlash_Class::Log_Write_ESC(), DataFlash_Class::Log_Write_IMU_instance(), loop(), AP_Baro::setHIL(), AP_Baro_FBM320::timer(), AP_Baro_DPS280::timer(), AP_Baro_BMP085::update(), AP_Baro_KellerLD::update(), AP_Airspeed_MS4525::~AP_Airspeed_MS4525(), and AP_Airspeed_SDP3X::~AP_Airspeed_SDP3X().