AP_Declination_test.cpp File Reference

#include <AP_HAL/AP_HAL.h>
#include <AP_Common/AP_Common.h>
#include <AP_Param/AP_Param.h>
#include <StorageManager/StorageManager.h>
#include <AP_Math/AP_Math.h>
#include <AP_Declination/AP_Declination.h>
#include <AP_Buffer/AP_Buffer.h>
#include <Filter/Filter.h>

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Functions
void	setup ()
void	loop ()
static float	get_declination (float lat, float lon)
	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...
static const int16_t	dec_tbl [37][73]

Function Documentation

AP_HAL_MAIN()

AP_HAL_MAIN

(

)

Referenced by loop().

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get_declination()

static float get_declination ( float  lat, float  lon  )

static

Definition at line 57 of file AP_Declination_test.cpp.

Referenced by setup().

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loop()

void loop

(

void

)

Definition at line 108 of file AP_Declination_test.cpp.

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setup()

void setup

(

void

)

Definition at line 79 of file AP_Declination_test.cpp.

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Variable Documentation

dec_tbl

const int16_t dec_tbl[37][73]

static

Definition at line 16 of file AP_Declination_test.cpp.

Referenced by get_declination().

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 14 of file AP_Declination_test.cpp.