#include <AP_HAL/AP_HAL.h>

Include dependency graph for RCInputToRCOutput.cpp:

Macros
#define	MAX_CHANNELS 14

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...

static uint8_t	max_channels = 0

static uint16_t	last_value [MAX_CHANNELS]

Macro Definition Documentation

◆ MAX_CHANNELS

#define MAX_CHANNELS 14

Definition at line 14 of file RCInputToRCOutput.cpp.

Referenced by loop(), and setup().

Function Documentation

◆ AP_HAL_MAIN()

AP_HAL_MAIN ( )

Referenced by loop().

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◆ loop()

void loop ( void )

Definition at line 28 of file RCInputToRCOutput.cpp.

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◆ setup()

void setup ( void )

Definition at line 19 of file RCInputToRCOutput.cpp.

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Variable Documentation

◆ 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 12 of file RCInputToRCOutput.cpp.

◆ last_value

uint16_t last_value[MAX_CHANNELS]

static

Definition at line 17 of file RCInputToRCOutput.cpp.

Referenced by loop().

◆ max_channels

uint8_t max_channels = 0

static

Definition at line 16 of file RCInputToRCOutput.cpp.

Referenced by dsm_decode(), and loop().

Macros

Functions

Variables