ardupilot/ArduCopterMega/ArduCopterMega.pde

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

/*
ArduCopter Version 2.0 Beta
Authors:	Jason Short
Based on code and ideas from the Arducopter team: Jose Julio, Randy Mackay, Jani Hirvinen
Thanks to:	Chris Anderson, Mike Smith, Jordi Munoz, Doug Weibel, James Goppert, Benjamin Pelletier


This firmware is free software; you can redistribute it and/or
modify it under the terms of the GNU Lesser General Public
License as published by the Free Software Foundation; either
version 2.1 of the License, or (at your option) any later version.

Special Thanks for Contributors:

Hein Hollander 		:Octo Support
Dani Saez 			:V Ocoto Support
Max Levine			:Tri Support, Graphics
Jose Julio			:Stabilization Control laws
Randy MacKay		:Heli Support
Jani Hiriven		:Testing feedback
Andrew Tridgell		:Mavlink Support
James Goppert		:Mavlink Support
Doug Weibel			:Libraries
Mike Smith			:Libraries, Coding support
HappyKillmore		:Mavlink GCS
Micheal Oborne		:Mavlink GCS
Jack Dunkle			:Alpha testing
Christof Schmid		:Alpha testing
Guntars				:Arming safety suggestion

And much more so PLEASE PM me on DIYDRONES to add your contribution to the List

*/

////////////////////////////////////////////////////////////////////////////////
// Header includes
////////////////////////////////////////////////////////////////////////////////

// AVR runtime
#include <avr/io.h>
#include <avr/eeprom.h>
#include <avr/pgmspace.h>
#include <math.h>

// Libraries
#include <FastSerial.h>
#include <AP_Common.h>
#include <APM_RC.h>         // ArduPilot Mega RC Library
#include <AP_GPS.h>         // ArduPilot GPS library
#include <Wire.h>			// Arduino I2C lib
#include <SPI.h>
#include <DataFlash.h>      // ArduPilot Mega Flash Memory Library
#include <AP_ADC.h>         // ArduPilot Mega Analog to Digital Converter Library
#include <APM_BMP085.h>     // ArduPilot Mega BMP085 Library
#include <AP_Compass.h>     // ArduPilot Mega Magnetometer Library
#include <AP_Math.h>        // ArduPilot Mega Vector/Matrix math Library
#include <AP_IMU.h>         // ArduPilot Mega IMU Library
#include <AP_DCM.h>         // ArduPilot Mega DCM Library
#include <PID.h>            // PID library
#include <RC_Channel.h>     // RC Channel Library
#include <AP_RangeFinder.h>	// Range finder library
#include <AP_OpticalFlow.h> // Optical Flow library
#include <ModeFilter.h>

#define MAVLINK_COMM_NUM_BUFFERS 2
#include <GCS_MAVLink.h>    // MAVLink GCS definitions

// Configuration
#include "defines.h"
#include "config.h"

// Local modules
#include "Parameters.h"
#include "GCS.h"
#include "HIL.h"

////////////////////////////////////////////////////////////////////////////////
// Serial ports
////////////////////////////////////////////////////////////////////////////////
//
// Note that FastSerial port buffers are allocated at ::begin time,
// so there is not much of a penalty to defining ports that we don't
// use.
//
FastSerialPort0(Serial);        // FTDI/console
FastSerialPort1(Serial1);       // GPS port
FastSerialPort3(Serial3);       // Telemetry port

////////////////////////////////////////////////////////////////////////////////
// Parameters
////////////////////////////////////////////////////////////////////////////////
//
// Global parameters are all contained within the 'g' class.
//
static Parameters      g;


////////////////////////////////////////////////////////////////////////////////
// prototypes
static void update_events(void);


////////////////////////////////////////////////////////////////////////////////
// Sensors
////////////////////////////////////////////////////////////////////////////////
//
// There are three basic options related to flight sensor selection.
//
// - Normal flight mode.  Real sensors are used.
// - HIL Attitude mode.  Most sensors are disabled, as the HIL
//   protocol supplies attitude information directly.
// - HIL Sensors mode.  Synthetic sensors are configured that
//   supply data from the simulation.
//

// All GPS access should be through this pointer.
static GPS         *g_gps;

// flight modes convenience array
static AP_Int8                *flight_modes = &g.flight_mode1;

#if HIL_MODE == HIL_MODE_DISABLED

	// real sensors
	AP_ADC_ADS7844          adc;
	APM_BMP085_Class        barometer;
    AP_Compass_HMC5843      compass(Parameters::k_param_compass);

  #ifdef OPTFLOW_ENABLED
    AP_OpticalFlow_ADNS3080 optflow;
  #endif

	// real GPS selection
	#if   GPS_PROTOCOL == GPS_PROTOCOL_AUTO
		AP_GPS_Auto     g_gps_driver(&Serial1, &g_gps);

	#elif GPS_PROTOCOL == GPS_PROTOCOL_NMEA
		AP_GPS_NMEA     g_gps_driver(&Serial1);

	#elif GPS_PROTOCOL == GPS_PROTOCOL_SIRF
		AP_GPS_SIRF     g_gps_driver(&Serial1);

	#elif GPS_PROTOCOL == GPS_PROTOCOL_UBLOX
		AP_GPS_UBLOX    g_gps_driver(&Serial1);

	#elif GPS_PROTOCOL == GPS_PROTOCOL_MTK
		AP_GPS_MTK      g_gps_driver(&Serial1);

	#elif GPS_PROTOCOL == GPS_PROTOCOL_MTK16
		AP_GPS_MTK16    g_gps_driver(&Serial1);

	#elif GPS_PROTOCOL == GPS_PROTOCOL_NONE
		AP_GPS_None     g_gps_driver(NULL);

	#else
		#error Unrecognised GPS_PROTOCOL setting.
	#endif // GPS PROTOCOL

#elif HIL_MODE == HIL_MODE_SENSORS
	// sensor emulators
	AP_ADC_HIL              adc;
	APM_BMP085_HIL_Class    barometer;
	AP_Compass_HIL          compass;
	AP_GPS_HIL              g_gps_driver(NULL);

#elif HIL_MODE == HIL_MODE_ATTITUDE
	AP_ADC_HIL              adc;
	AP_DCM_HIL              dcm;
	AP_GPS_HIL              g_gps_driver(NULL);
	AP_Compass_HIL          compass; // never used
	AP_IMU_Shim             imu; // never used
	#ifdef OPTFLOW_ENABLED
		AP_OpticalFlow_ADNS3080 optflow;
	#endif
    static int32_t          gps_base_alt;
#else
	#error Unrecognised HIL_MODE setting.
#endif // HIL MODE

#if HIL_MODE != HIL_MODE_DISABLED
	#if HIL_PROTOCOL == HIL_PROTOCOL_MAVLINK
		GCS_MAVLINK	hil(Parameters::k_param_streamrates_port0);
	#elif HIL_PROTOCOL == HIL_PROTOCOL_XPLANE
		HIL_XPLANE hil;
	#endif // HIL PROTOCOL
#endif // HIL_MODE

//  We may have a hil object instantiated just for mission planning
#if HIL_MODE == HIL_MODE_DISABLED && HIL_PROTOCOL == HIL_PROTOCOL_MAVLINK && HIL_PORT == 0
	GCS_MAVLINK	hil(Parameters::k_param_streamrates_port0);
#endif

#if HIL_MODE != HIL_MODE_ATTITUDE
	#if HIL_MODE != HIL_MODE_SENSORS
		// Normal
		AP_IMU_Oilpan imu(&adc, Parameters::k_param_IMU_calibration);
	#else
		// hil imu
		AP_IMU_Shim imu;
	#endif
	// normal dcm
	AP_DCM  dcm(&imu, g_gps);
#endif

////////////////////////////////////////////////////////////////////////////////
// GCS selection
////////////////////////////////////////////////////////////////////////////////
//
#if   GCS_PROTOCOL == GCS_PROTOCOL_MAVLINK
	GCS_MAVLINK	gcs(Parameters::k_param_streamrates_port3);
#else
	// If we are not using a GCS, we need a stub that does nothing.
	GCS_Class           gcs;
#endif

//#include <GCS_SIMPLE.h>
//GCS_SIMPLE    gcs_simple(&Serial);

////////////////////////////////////////////////////////////////////////////////
// SONAR selection
////////////////////////////////////////////////////////////////////////////////
//
ModeFilter sonar_mode_filter;

#if SONAR_TYPE == MAX_SONAR_XL
	AP_RangeFinder_MaxsonarXL sonar(&adc, &sonar_mode_filter);//(SONAR_PORT, &adc);
#elif SONAR_TYPE == MAX_SONAR_LV
	// XXX honestly I think these output the same values
	// If someone knows, can they confirm it?
	AP_RangeFinder_MaxsonarXL sonar(&adc, &sonar_mode_filter);//(SONAR_PORT, &adc);
#endif

////////////////////////////////////////////////////////////////////////////////
// Global variables
////////////////////////////////////////////////////////////////////////////////
static const char *comma = ",";

static const char* flight_mode_strings[] = {
	"STABILIZE",
	"ACRO",
	"SIMPLE",
	"ALT_HOLD",
	"AUTO",
	"GUIDED",
	"LOITER",
	"RTL",
	"CIRCLE"};

/* Radio values
		Channel assignments
			1	Ailerons (rudder if no ailerons)
			2	Elevator
			3	Throttle
			4	Rudder (if we have ailerons)
			5	Mode - 3 position switch
			6 	User assignable
			7	trainer switch - sets throttle nominal (toggle switch), sets accels to Level (hold > 1 second)
			8	TBD
*/

// test
//Vector3f accels_rot;
//float	accel_gain = 20;


// Radio
// -----
static byte 		control_mode		= STABILIZE;
static byte 		old_control_mode	= STABILIZE;
static byte 		oldSwitchPosition;					// for remembering the control mode switch
static int 		motor_out[8];

// Heli
// ----
#if FRAME_CONFIG ==	HELI_FRAME
static float heli_rollFactor[3], heli_pitchFactor[3];  // only required for 3 swashplate servos
static int heli_servo_min[3], heli_servo_max[3];       // same here.  for yaw servo we use heli_servo4_min/max parameter directly
static int heli_servo_out[4];
#endif

// Failsafe
// --------
static boolean 	failsafe;						// did our throttle dip below the failsafe value?
static boolean 	ch3_failsafe;
static boolean		motor_armed;
static boolean		motor_auto_armed;				// if true,

// PIDs
// ----
//int 	max_stabilize_dampener;				//
//int 	max_yaw_dampener;					//
static boolean rate_yaw_flag;						// used to transition yaw control from Rate control to Yaw hold
static byte 	yaw_debug;
static bool 	did_clear_yaw_control;
static Vector3f omega;

// LED output
// ----------
static boolean motor_light;						// status of the Motor safety
static boolean GPS_light;							// status of the GPS light
static boolean timer_light;						// status of the Motor safety
static byte	led_mode = NORMAL_LEDS;

// GPS variables
// -------------
static const 	float t7			= 10000000.0;	// used to scale GPS values for EEPROM storage
static float 	scaleLongUp			= 1;			// used to reverse longtitude scaling
static float 	scaleLongDown 		= 1;			// used to reverse longtitude scaling
static byte 	ground_start_count	= 10;			// have we achieved first lock and set Home?
static bool 	did_ground_start	= false;		// have we ground started after first arming

// Location & Navigation
// ---------------------
static const float radius_of_earth 	= 6378100;		// meters
static const float gravity 			= 9.81;			// meters/ sec^2
static long		nav_bearing;						// deg * 100 : 0 to 360 current desired bearing to navigate
static long		target_bearing;						// deg * 100 : 0 to 360 location of the plane to the target
static long		crosstrack_bearing;					// deg * 100 : 0 to 360 desired angle of plane to target
static int		climb_rate;							// m/s * 100  - For future implementation of controlled ascent/descent by rate
static float	nav_gain_scaler 		= 1;		// Gain scaling for headwind/tailwind TODO: why does this variable need to be initialized to 1?

static int 	last_ground_speed;					// used to dampen navigation
static int	waypoint_speed;

static byte	wp_control;							// used to control - navgation or loiter

static byte	command_must_index;					// current command memory location
static byte	command_may_index;					// current command memory location
static byte	command_must_ID;					// current command ID
static byte	command_may_ID;						// current command ID
static byte wp_verify_byte;						// used for tracking state of navigating waypoints

static float cos_roll_x 	= 1;
static float cos_pitch_x 	= 1;
static float cos_yaw_x 	= 1;
static float sin_pitch_y, sin_yaw_y, sin_roll_y;
static bool simple_bearing_is_set = false;
static long initial_simple_bearing;				// used for Simple mode

// Acro
#if CH7_OPTION == DO_FLIP
static bool do_flip = false;
#endif

// Airspeed
// --------
static int		airspeed;							// m/s * 100

// Location Errors
// ---------------
static long		bearing_error;						// deg * 100 : 0 to 36000
static long		altitude_error;						// meters * 100 we are off in altitude
static float	crosstrack_error;					// meters we are off trackline
static long 	distance_error;						// distance to the WP
static long 	yaw_error;							// how off are we pointed
static long		long_error, lat_error;				// temp for debugging
static int		loiter_error_max;

// Battery Sensors
// ---------------
static float	battery_voltage		= LOW_VOLTAGE * 1.05;		// Battery Voltage of total battery, initialized above threshold for filter
static float 	battery_voltage1 	= LOW_VOLTAGE * 1.05;		// Battery Voltage of cell 1, initialized above threshold for filter
static float 	battery_voltage2 	= LOW_VOLTAGE * 1.05;		// Battery Voltage of cells 1 + 2, initialized above threshold for filter
static float 	battery_voltage3 	= LOW_VOLTAGE * 1.05;		// Battery Voltage of cells 1 + 2+3, initialized above threshold for filter
static float 	battery_voltage4 	= LOW_VOLTAGE * 1.05;		// Battery Voltage of cells 1 + 2+3 + 4, initialized above threshold for filter

static float	current_amps;
static float	current_total;
static bool		low_batt = false;

// Airspeed Sensors
// ----------------

// Barometer Sensor variables
// --------------------------
static long 	abs_pressure;
static long 	ground_pressure;
static int 		ground_temperature;
static int32_t 	baro_filter[BARO_FILTER_SIZE];
static byte		baro_filter_index;

// Altitude Sensor variables
// ----------------------
static int		sonar_alt;
static int		baro_alt;
static int		baro_alt_offset;
static byte 	altitude_sensor = BARO;				// used to know which sensor is active, BARO or SONAR


// flight mode specific
// --------------------
static boolean	takeoff_complete;					// Flag for using take-off controls
static boolean	land_complete;
//static int		takeoff_altitude;
static int		landing_distance;					// meters;
static long 	old_alt;							// used for managing altitude rates
static int		velocity_land;
static byte 	yaw_tracking = MAV_ROI_WPNEXT;		// no tracking, point at next wp, or at a target
//static int		throttle_slew;						// used to smooth throttle tranistions

// Loiter management
// -----------------
static long 	saved_target_bearing;				// deg * 100
static unsigned long 	loiter_time;				// millis : when we started LOITER mode
static unsigned long 	loiter_time_max;			// millis : how long to stay in LOITER mode

// these are the values for navigation control functions
// ----------------------------------------------------
static long		nav_roll;							// deg * 100 : target roll angle
static long		nav_pitch;							// deg * 100 : target pitch angle
static long		nav_yaw;							// deg * 100 : target yaw angle
static long		nav_lat;							// for error calcs
static long		nav_lon;							// for error calcs
static int		nav_throttle;						// 0-1000 for throttle control

static long 	throttle_integrator;				// used to control when we calculate nav_throttle
static bool 	invalid_throttle;					// used to control when we calculate nav_throttle
static bool 	set_throttle_cruise_flag = false;	// used to track the throttle crouse value

static long 	command_yaw_start;					// what angle were we to begin with
static unsigned long 	command_yaw_start_time;				// when did we start turning
static unsigned int	command_yaw_time;					// how long we are turning
static long 	command_yaw_end;					// what angle are we trying to be
static long 	command_yaw_delta;					// how many degrees will we turn
static int		command_yaw_speed;					// how fast to turn
static byte		command_yaw_dir;
static byte		command_yaw_relative;

static int 	auto_level_counter;

// Waypoints
// ---------
static long	wp_distance;						// meters - distance between plane and next waypoint
static long	wp_totalDistance;					// meters - distance between old and next waypoint
static byte	next_wp_index;						// Current active command index

// repeating event control
// -----------------------
static byte 	event_id; 							// what to do - see defines
static unsigned long 	event_timer; 						// when the event was asked for in ms
static unsigned int 	event_delay; 						// how long to delay the next firing of event in millis
static int 		event_repeat;						// how many times to fire : 0 = forever, 1 = do once, 2 = do twice
static int 		event_value; 						// per command value, such as PWM for servos
static int 		event_undo_value;					// the value used to undo commands
static byte 	repeat_forever;
static byte 	undo_event;							// counter for timing the undo

// delay command
// --------------
static long 	condition_value;					// used in condition commands (eg delay, change alt, etc.)
static long 	condition_start;
static int 		condition_rate;

// land command
// ------------
static long 	land_start;							// when we intiated command in millis()
static long 	original_alt;						// altitide reference for start of command

// 3D Location vectors
// -------------------
static struct 	Location home;						// home location
static struct 	Location prev_WP;					// last waypoint
static struct 	Location current_loc;				// current location
static struct 	Location next_WP;					// next waypoint
static struct 	Location target_WP;					// where do we want to you towards?
static struct 	Location simple_WP;					//
static struct 	Location next_command;				// command preloaded
static struct   Location guided_WP;					// guided mode waypoint
static long 	target_altitude;					// used for
static boolean	home_is_set; 						// Flag for if we have g_gps lock and have set the home location
static struct	Location optflow_offset;			// optical flow base position
static boolean  new_location;						// flag to tell us if location has been updated


// IMU variables
// -------------
static float G_Dt						= 0.02;		// Integration time for the gyros (DCM algorithm)


// Performance monitoring
// ----------------------
static long 	perf_mon_timer;
static float 	imu_health; 						// Metric based on accel gain deweighting
static int 	G_Dt_max;							// Max main loop cycle time in milliseconds
static int 	gps_fix_count;
static byte	gcs_messages_sent;


// GCS
// ---
static char GCS_buffer[53];
static char display_PID = -1;						// Flag used by DebugTerminal to indicate that the next PID calculation with this index should be displayed

// System Timers
// --------------
static unsigned long 	fast_loopTimer;				// Time in miliseconds of main control loop
static unsigned long 	fast_loopTimeStamp;			// Time Stamp when fast loop was complete
static uint8_t 		delta_ms_fast_loop; 		// Delta Time in miliseconds
static int 			mainLoop_count;

static unsigned long 	medium_loopTimer;			// Time in miliseconds of navigation control loop
static byte 			medium_loopCounter;			// Counters for branching from main control loop to slower loops
static uint8_t			delta_ms_medium_loop;

static unsigned long	fiftyhz_loopTimer;
static uint8_t			delta_ms_fiftyhz;

static byte 			slow_loopCounter;
static int 			superslow_loopCounter;
static byte			flight_timer;				// for limiting the execution of flight mode thingys


static unsigned long 	dTnav;						// Delta Time in milliseconds for navigation computations
static unsigned long 	nav_loopTimer;				// used to track the elapsed ime for GPS nav
static unsigned long 	elapsedTime;				// for doing custom events
static float 			load;						// % MCU cycles used

static byte			counter_one_herz;
static bool			GPS_enabled 	= false;
static byte			loop_step;

////////////////////////////////////////////////////////////////////////////////
// Top-level logic
////////////////////////////////////////////////////////////////////////////////

void setup() {
	init_ardupilot();
}

void loop()
{
	// We want this to execute fast
	// ----------------------------
	if (millis() - fast_loopTimer >= 5) {
		//PORTK |= B00010000;
		delta_ms_fast_loop 	= millis() - fast_loopTimer;
		fast_loopTimer		= millis();
		load				= float(fast_loopTimeStamp - fast_loopTimer) / delta_ms_fast_loop;
		G_Dt 				= (float)delta_ms_fast_loop / 1000.f;		// used by DCM integrator
		mainLoop_count++;

		//if (delta_ms_fast_loop > 6)
		//	Log_Write_Performance();

		// Execute the fast loop
		// ---------------------
		fast_loop();
		fast_loopTimeStamp = millis();
	}

	if (millis() - fiftyhz_loopTimer > 19) {
		delta_ms_fiftyhz 		= millis() - fiftyhz_loopTimer;
		fiftyhz_loopTimer		= millis();
		//PORTK |= B01000000;

		// reads all of the necessary trig functions for cameras, throttle, etc.
		update_trig();

		medium_loop();

		// Stuff to run at full 50hz, but after the loops
		fifty_hz_loop();

		counter_one_herz++;

		if(counter_one_herz == 50){
			super_slow_loop();
			counter_one_herz = 0;
		}

		if (millis() - perf_mon_timer > 20000) {
			if (mainLoop_count != 0) {

				gcs.send_message(MSG_PERF_REPORT);

				if (g.log_bitmask & MASK_LOG_PM)
					Log_Write_Performance();

                resetPerfData();
            }
        }
		//PORTK &= B10111111;
	}
	//PORTK &= B11101111;
}
//  PORTK |= B01000000;
//	PORTK &= B10111111;

// Main loop
static void fast_loop()
{
	// IMU DCM Algorithm
	read_AHRS();

	// This is the fast loop - we want it to execute at >= 100Hz
	// ---------------------------------------------------------
	if (delta_ms_fast_loop > G_Dt_max)
		G_Dt_max = delta_ms_fast_loop;

	// Read radio
	// ----------
	read_radio();

	// custom code/exceptions for flight modes
	// ---------------------------------------
	update_current_flight_mode();

	// write out the servo PWM values
	// ------------------------------
	set_servos_4();
}

static void medium_loop()
{
	// This is the start of the medium (10 Hz) loop pieces
	// -----------------------------------------
	switch(medium_loopCounter) {

		// This case deals with the GPS and Compass
		//-----------------------------------------
		case 0:
			loop_step = 1;

			medium_loopCounter++;

			if(GPS_enabled){
				update_GPS();
			}

			//readCommands();

			#if HIL_MODE != HIL_MODE_ATTITUDE
				if(g.compass_enabled){
					compass.read();		 						// Read magnetometer
					compass.calculate(dcm.get_dcm_matrix());  	// Calculate heading
					compass.null_offsets(dcm.get_dcm_matrix());
				}
			#endif

			// auto_trim, uses an auto_level algorithm
			auto_trim();
			break;

		// This case performs some navigation computations
		//------------------------------------------------
		case 1:
			loop_step = 2;
			medium_loopCounter++;

			// hack to stop navigation in Simple mode
			if (control_mode == SIMPLE){
				// clear GPS data
				g_gps->new_data = false;
				break;
			}

			// Auto control modes:
			if(g_gps->new_data && g_gps->fix){
				loop_step = 11;

				// invalidate GPS data
				g_gps->new_data 	= false;

				// we are not tracking I term on navigation, so this isn't needed
				dTnav 				= millis() - nav_loopTimer;
				nav_loopTimer 		= millis();

				// calculate the copter's desired bearing and WP distance
				// ------------------------------------------------------
				navigate();

				// control mode specific updates to nav_bearing
				// --------------------------------------------
				update_navigation();

				if (g.log_bitmask & MASK_LOG_NTUN)
					Log_Write_Nav_Tuning();
			}

			break;

		// command processing
		//-------------------
		case 2:
			loop_step = 3;
			medium_loopCounter++;

			// Read altitude from sensors
			// --------------------------
			update_alt();

			// altitude smoothing
			// ------------------
			//calc_altitude_smoothing_error();

			calc_altitude_error();

			// invalidate the throttle hold value
			// ----------------------------------
			invalid_throttle = true;
			break;

		// This case deals with sending high rate telemetry
		//-------------------------------------------------
		case 3:
			loop_step = 4;
			medium_loopCounter++;

			// perform next command
			// --------------------
			if(control_mode == AUTO){
				update_commands();
			}

			#if HIL_MODE != HIL_MODE_ATTITUDE
				if (g.log_bitmask & MASK_LOG_ATTITUDE_MED)
					Log_Write_Attitude();

				if (g.log_bitmask & MASK_LOG_CTUN)
					Log_Write_Control_Tuning();
			#endif

			#if GCS_PROTOCOL == GCS_PROTOCOL_MAVLINK
				gcs.data_stream_send(5,45);
				// send all requested output streams with rates requested
				// between 5 and 45 Hz
			#else
				gcs.send_message(MSG_ATTITUDE);     // Sends attitude data
			#endif

			#if HIL_PROTOCOL == HIL_PROTOCOL_MAVLINK && (HIL_MODE != HIL_MODE_DISABLED || HIL_PORT == 0)
				hil.data_stream_send(5,45);
			#endif

			if (g.log_bitmask & MASK_LOG_MOTORS)
				Log_Write_Motors();

			break;

		// This case controls the slow loop
		//---------------------------------
		case 4:
			loop_step = 5;
			medium_loopCounter = 0;

			delta_ms_medium_loop	= millis() - medium_loopTimer;
			medium_loopTimer    	= millis();

			if (g.battery_monitoring != 0){
				read_battery();
			}

			// Accel trims 		= hold > 2 seconds
			// Throttle cruise  = switch less than 1 second
			// --------------------------------------------
			read_trim_switch();

			// Check for engine arming
			// -----------------------
			arm_motors();


			slow_loop();
			break;

		default:
			// this is just a catch all
			// ------------------------
			medium_loopCounter = 0;
			break;
	}

}

// stuff that happens at 50 hz
// ---------------------------
static void fifty_hz_loop()
{
	// record throttle output
	// ------------------------------
	throttle_integrator += g.rc_3.servo_out;

	// Read Sonar
	// ----------
	if(g.sonar_enabled){
		sonar_alt 			= sonar.read();
	}

	#if HIL_PROTOCOL == HIL_PROTOCOL_MAVLINK && HIL_MODE != HIL_MODE_DISABLED
		// HIL for a copter needs very fast update of the servo values
		hil.send_message(MSG_RADIO_OUT);
	#endif

	// use Yaw to find our bearing error
	calc_bearing_error();

	//if (throttle_slew < 0)
	//	throttle_slew++;
	//else if (throttle_slew > 0)
	//	throttle_slew--;

	//throttle_slew = min((800 - g.rc_3.control_in), throttle_slew);

	# if HIL_MODE == HIL_MODE_DISABLED
		if (g.log_bitmask & MASK_LOG_ATTITUDE_FAST)
			Log_Write_Attitude();

		if (g.log_bitmask & MASK_LOG_RAW)
			Log_Write_Raw();
	#endif

	//#if CAMERA_STABILIZER == ENABLED
		camera_stabilization();
	//#endif


	#if HIL_MODE != HIL_MODE_DISABLED && HIL_PORT != GCS_PORT
		// kick the HIL to process incoming sensor packets
		hil.update();

		#if HIL_PROTOCOL == HIL_PROTOCOL_MAVLINK
			hil.data_stream_send(45,1000);
		#else
			hil.send_message(MSG_SERVO_OUT);
		#endif
	#elif HIL_PROTOCOL == HIL_PROTOCOL_MAVLINK && HIL_MODE == HIL_MODE_DISABLED && HIL_PORT == 0
		// Case for hil object on port 0 just for mission planning
		hil.update();
		hil.data_stream_send(45,1000);
	#endif

	// kick the GCS to process uplink data
	gcs.update();

	#if GCS_PROTOCOL == GCS_PROTOCOL_MAVLINK
		gcs.data_stream_send(45,1000);
	#endif

	#if FRAME_CONFIG == TRI_FRAME
		// servo Yaw
		g.rc_4.calc_pwm();
		APM_RC.OutputCh(CH_7, g.rc_4.radio_out);
	#endif
}


static void slow_loop()
{
	// This is the slow (3 1/3 Hz) loop pieces
	//----------------------------------------
	switch (slow_loopCounter){
		case 0:
			loop_step = 6;
			slow_loopCounter++;
			superslow_loopCounter++;

			if(superslow_loopCounter > 800){ // every 4 minutes
				#if HIL_MODE != HIL_MODE_ATTITUDE
					if(g.rc_3.control_in == 0 && g.compass_enabled){
						compass.save_offsets();
						superslow_loopCounter = 0;
					}
				#endif
            }
			break;

		case 1:
			loop_step = 7;
			slow_loopCounter++;

			// Read 3-position switch on radio
			// -------------------------------
			read_control_switch();

			// Read main battery voltage if hooked up - does not read the 5v from radio
			// ------------------------------------------------------------------------
			//#if BATTERY_EVENT == 1
			//	read_battery();
			//#endif

			#if AUTO_RESET_LOITER == 1
			if(control_mode == LOITER){
				if((abs(g.rc_2.control_in) + abs(g.rc_1.control_in)) > 1500){
					// reset LOITER to current position
					//long temp 	= next_WP.alt;
					next_WP 	= current_loc;
					//next_WP.alt = temp;
				}
			}
			#endif

			break;

		case 2:
			loop_step = 8;
			slow_loopCounter = 0;
			update_events();

			// blink if we are armed
			update_lights();

			#if GCS_PROTOCOL == GCS_PROTOCOL_MAVLINK
				gcs.data_stream_send(1,5);
				// send all requested output streams with rates requested
				// between 1 and 5 Hz
			#else
				gcs.send_message(MSG_LOCATION);
				gcs.send_message(MSG_CPU_LOAD, load*100);
			#endif

			#if HIL_PROTOCOL == HIL_PROTOCOL_MAVLINK && (HIL_MODE != HIL_MODE_DISABLED || HIL_PORT == 0)
				hil.data_stream_send(1,5);
			#endif

			#if CHANNEL_6_TUNING != CH6_NONE
				tuning();
			#endif

			// filter out the baro offset.
			//if(baro_alt_offset > 0) baro_alt_offset--;
			//if(baro_alt_offset < 0) baro_alt_offset++;


			#if MOTOR_LEDS == 1
				update_motor_leds();
			#endif

			break;

		default:
			slow_loopCounter = 0;
			break;

	}
}

// 1Hz loop
static void super_slow_loop()
{
	loop_step = 9;
	if (g.log_bitmask & MASK_LOG_CUR)
		Log_Write_Current();

    gcs.send_message(MSG_HEARTBEAT);

	#if HIL_PROTOCOL == HIL_PROTOCOL_MAVLINK && (HIL_MODE != HIL_MODE_DISABLED || HIL_PORT == 0)
		hil.send_message(MSG_HEARTBEAT);
	#endif
}

static void update_GPS(void)
{
	loop_step = 10;
	g_gps->update();
	update_GPS_light();

	//current_loc.lng =   377697000;		// Lon * 10 * *7
	//current_loc.lat = -1224318000;		// Lat * 10 * *7
	//current_loc.alt = 100;				// alt * 10 * *7
	//return;

    if (g_gps->new_data && g_gps->fix) {

		// XXX We should be sending GPS data off one of the regular loops so that we send
		// no-GPS-fix data too
		#if GCS_PROTOCOL != GCS_PROTOCOL_MAVLINK
			gcs.send_message(MSG_LOCATION);
		#endif

		// for performance
		// ---------------
		gps_fix_count++;

		if(ground_start_count > 1){
			ground_start_count--;

		} else if (ground_start_count == 1) {

			// We countdown N number of good GPS fixes
			// so that the altitude is more accurate
			// -------------------------------------
			if (current_loc.lat == 0) {
                SendDebugln("!! bad loc");
				ground_start_count = 5;

			}else{
				//Serial.printf("init Home!");

				// reset our nav loop timer
				//nav_loopTimer = millis();
				init_home();

				// init altitude
				// commented out because we aren't using absolute altitude
				// current_loc.alt = home.alt;
				ground_start_count = 0;
			}
		}

		current_loc.lng = g_gps->longitude;	// Lon * 10 * *7
		current_loc.lat = g_gps->latitude;	// Lat * 10 * *7

		if (g.log_bitmask & MASK_LOG_GPS){
			Log_Write_GPS();
		}
	}
}

#ifdef OPTFLOW_ENABLED
// blend gps and optical flow location
void update_location(void)
{
    //static int count = 0;
    // get GPS position
	if(GPS_enabled){
		update_GPS();
	}

	if( g.optflow_enabled ) {
	    int32_t	temp_lat, temp_lng, diff_lat, diff_lng;

		// get optical flow position
		optflow.read();
		optflow.get_position(dcm.roll, dcm.pitch, dcm.yaw, current_loc.alt-home.alt);

		// write to log
		if (g.log_bitmask & MASK_LOG_OPTFLOW){
			Log_Write_Optflow();
		}

		temp_lat = optflow_offset.lat + optflow.lat;
		temp_lng = optflow_offset.lng + optflow.lng;

		// if we have good GPS values, don't let optical flow position stray too far
		if( GPS_enabled && g_gps->fix ) {
			// ensure current location is within 3m of gps location
			diff_lat = g_gps->latitude - temp_lat;
			diff_lng = g_gps->longitude - temp_lng;
			if( diff_lat > 300 ) {
				optflow_offset.lat += diff_lat - 300;
				//Serial.println("lat inc!");
			}
			if( diff_lat < -300 ) {
				optflow_offset.lat += diff_lat + 300;
				//Serial.println("lat dec!");
			}
			if( diff_lng > 300 ) {
				optflow_offset.lng += diff_lng - 300;
				//Serial.println("lng inc!");
			}
			if( diff_lng < -300 ) {
				optflow_offset.lng += diff_lng + 300;
				//Serial.println("lng dec!");
			}
		}

		// update the current position
		current_loc.lat = optflow_offset.lat + optflow.lat;
		current_loc.lng = optflow_offset.lng + optflow.lng;

		/*count++;
		if( count >= 20 ) {
		    count = 0;
			Serial.println();
			Serial.print("lat:");
			Serial.print(current_loc.lat);
			Serial.print("\tlng:");
			Serial.print(current_loc.lng);
			Serial.print("\tr:");
			Serial.print(nav_roll);
			Serial.print("\tp:");
			Serial.print(nav_pitch);
			Serial.println();
		}*/

		// indicate we have a new position for nav functions
		new_location = true;

	}else{
	    // get current position from gps
		current_loc.lng = g_gps->longitude;	// Lon * 10 * *7
		current_loc.lat = g_gps->latitude;	// Lat * 10 * *7

		new_location = g_gps->new_data;
	}
}
#endif


void update_current_flight_mode(void)
{
	#if CH7_OPTION == DO_FLIP
	if (do_flip){
		roll_flip();
		return;
	}
	#endif

	if(control_mode == AUTO){

		// this is a hack to prevent run up of the throttle I term for alt hold
		if(command_must_ID == MAV_CMD_NAV_TAKEOFF){
			invalid_throttle = (g.rc_3.control_in != 0);
			// make invalid_throttle false if we are waiting to take off.
		}

		switch(command_must_ID){
			default:
				// mix in user control with Nav control
				g.rc_1.servo_out = g.rc_1.control_mix(nav_roll);
				g.rc_2.servo_out = g.rc_2.control_mix(nav_pitch);

				// Roll control
				g.rc_1.servo_out = get_stabilize_roll(g.rc_1.servo_out);

				// Pitch control
				g.rc_2.servo_out = get_stabilize_pitch(g.rc_2.servo_out);

				// Throttle control
				if(invalid_throttle){
					auto_throttle();
				}

				// Yaw control
				g.rc_4.servo_out = get_stabilize_yaw(nav_yaw, .5);
				break;
		}

	}else{

		switch(control_mode){
			case ACRO:
				// Roll control
				g.rc_1.servo_out = get_rate_roll(g.rc_1.control_in);

				// Pitch control
				g.rc_2.servo_out = get_rate_pitch(g.rc_2.control_in);

				// Throttle control
				g.rc_3.servo_out = get_throttle(g.rc_3.control_in);

				// Yaw control
				g.rc_4.servo_out = get_rate_yaw(g.rc_4.control_in);

				break;

			case STABILIZE:
				// calcualte new nav_yaw offset
				nav_yaw = get_nav_yaw_offset(g.rc_4.control_in, g.rc_3.control_in);

				// Roll control
				g.rc_1.servo_out = get_stabilize_roll(g.rc_1.control_in);

				// Pitch control
				g.rc_2.servo_out = get_stabilize_pitch(g.rc_2.control_in);

				// Throttle control
				g.rc_3.servo_out = get_throttle(g.rc_3.control_in);

				// Yaw control
				g.rc_4.servo_out = get_stabilize_yaw(nav_yaw, 1.0);

				//Serial.printf("%u\t%d\n", nav_yaw, g.rc_4.servo_out);
				break;

			case SIMPLE:
				flight_timer++;

				if(flight_timer > 6){
					flight_timer = 0;

					// make sure this is always 0
					simple_WP.lat = 0;
					simple_WP.lng = 0;

					next_WP.lng =  (float)g.rc_1.control_in * .9;  // X: 4500 * .7 = 2250 = 25 meteres
					next_WP.lat = -(float)g.rc_2.control_in * .9;  // Y: 4500 * .7 = 2250 = 25 meteres

					// calc a new bearing
					nav_bearing 	= get_bearing(&simple_WP, &next_WP) + initial_simple_bearing;
					nav_bearing 	= wrap_360(nav_bearing);
					wp_distance 	= get_distance(&simple_WP, &next_WP);

					calc_bearing_error();
					/*
					Serial.printf("lat: %ld lon:%ld, bear:%ld, dist:%ld, init:%ld, err:%ld ",
							next_WP.lat,
							next_WP.lng,
							nav_bearing,
							wp_distance,
							initial_simple_bearing,
							bearing_error);
					*/
					// get nav_pitch and nav_roll
					calc_simple_nav();
					calc_nav_output();
				}

				/*
				#if SIMPLE_LOOK_AT_HOME == 0
					// This is typical yaw behavior

					// are we at rest? reset nav_yaw
					if(g.rc_3.control_in == 0){
						clear_yaw_control();
					}else{
						// Yaw control
						output_manual_yaw();
					}
				#else
					// This is experimental,
					// copter will always point at home
					if(home_is_set)
						point_at_home_yaw();

					// Output Pitch, Roll, Yaw and Throttle
					// ------------------------------------
					auto_yaw();
				#endif
				*/

				// calcualte new nav_yaw offset
				nav_yaw = get_nav_yaw_offset(g.rc_4.control_in, g.rc_3.control_in);

				// Roll control
				g.rc_1.servo_out = get_stabilize_roll(nav_roll);

				// Pitch control
				g.rc_2.servo_out = get_stabilize_pitch(nav_pitch);

				// Throttle control
				g.rc_3.servo_out = get_throttle(g.rc_3.control_in);

				// Yaw control
				g.rc_4.servo_out = get_stabilize_yaw(nav_yaw, 1.0);
				//Serial.printf("%d \t %d\n", g.rc_3.servo_out, throttle_slew);

			break;

			case ALT_HOLD:
				// allow interactive changing of atitude
				adjust_altitude();

				// calcualte new nav_yaw offset
				nav_yaw = get_nav_yaw_offset(g.rc_4.control_in, 1); // send 1 instead of throttle to get nav control with low throttle

				// Roll control
				g.rc_1.servo_out = get_stabilize_roll(g.rc_1.control_in);

				// Pitch control
				g.rc_2.servo_out = get_stabilize_pitch(g.rc_2.control_in);

				// Throttle control
				if(invalid_throttle){
					auto_throttle();
				}

				// Yaw control
				g.rc_4.servo_out = get_stabilize_yaw(nav_yaw, 1.0);
				break;

			case CIRCLE:
			case GUIDED:
			case RTL:
				// mix in user control with Nav control
				g.rc_1.servo_out = g.rc_1.control_mix(nav_roll);
				g.rc_2.servo_out = g.rc_2.control_mix(nav_pitch);

				// Roll control
				g.rc_1.servo_out = get_stabilize_roll(g.rc_1.servo_out);

				// Pitch control
				g.rc_2.servo_out = get_stabilize_pitch(g.rc_2.servo_out);

				// Throttle control
				if(invalid_throttle){
					auto_throttle();
				}

				// Yaw control
				g.rc_4.servo_out = get_stabilize_yaw(nav_yaw, 0.25);
				break;

			case LOITER:
				// calcualte new nav_yaw offset
				nav_yaw = get_nav_yaw_offset(g.rc_4.control_in, 1); // send 1 instead of throttle to get nav control with low throttle

				// allow interactive changing of atitude
				adjust_altitude();

				// mix in user control with Nav control
				g.rc_1.servo_out = g.rc_1.control_mix(nav_roll);
				g.rc_2.servo_out = g.rc_2.control_mix(nav_pitch);

				// Roll control
				g.rc_1.servo_out = get_stabilize_roll(g.rc_1.servo_out);

				// Pitch control
				g.rc_2.servo_out = get_stabilize_pitch(g.rc_2.servo_out);

				// Throttle control
				if(invalid_throttle){
					auto_throttle();
				}

				// Yaw control
				g.rc_4.servo_out = get_stabilize_yaw(nav_yaw, 1.0);
				break;

			default:
				//Serial.print("$");
				break;
		}
	}
}

// called after a GPS read
static void update_navigation()
{
	// wp_distance is in ACTUAL meters, not the *100 meters we get from the GPS
	// ------------------------------------------------------------------------
	switch(control_mode){
		case AUTO:
			verify_commands();

			// note: wp_control is handled by commands_logic

			// calculates desired Yaw
			update_nav_yaw();

			// calculates the desired Roll and Pitch
			update_nav_wp();
			break;

		case GUIDED:
		case RTL:
			if(wp_distance > 5){
				// calculates desired Yaw
				// XXX this is an experiment
				#if FRAME_CONFIG ==	HELI_FRAME
				update_nav_yaw();
				#endif

			}

			//if(wp_distance < 4){
				// clears crosstrack
				crosstrack_bearing 	= target_bearing;
				//wp_control = WP_MODE;
			//}else{
				//wp_control = LOITER_MODE;
			//}

			wp_control = WP_MODE;

			// are we Traversing or Loitering?
			//wp_control = (wp_distance < 4 ) ? LOITER_MODE : WP_MODE;

			// calculates the desired Roll and Pitch
			//update_nav_wp();

			// calc a rate dampened pitch to the target
			calc_rate_nav(g.waypoint_speed_max.get());

			// rotate that pitch to the copter frame of reference
			calc_nav_output();

			//if(wp_distance < 4 )
			//	set_mode(LOITER);

			break;

			// switch passthrough to LOITER
		case LOITER:
			// are we Traversing or Loitering?
			//wp_control = (wp_distance < 20) ? LOITER_MODE : WP_MODE;
			wp_control = LOITER_MODE;

			// calculates the desired Roll and Pitch
			update_nav_wp();
			break;

		case CIRCLE:
			yaw_tracking = MAV_ROI_WPNEXT;
			// calculates desired Yaw
			update_nav_yaw();

			// hack to elmininate crosstrack effect
			crosstrack_bearing 	= target_bearing;

			// get a new nav_bearing
			update_loiter();

			// calc a rate dampened pitch to the target
			calc_rate_nav(400);

			// rotate that pitch to the copter frame of reference
			calc_nav_output();
			break;

	}
}

static void read_AHRS(void)
{
	// Perform IMU calculations and get attitude info
	//-----------------------------------------------
	#if HIL_MODE == HIL_MODE_SENSORS
		// update hil before dcm update
		hil.update();
	#endif

	dcm.update_DCM(G_Dt);
	omega = dcm.get_gyro();
}

static void update_trig(void){
	Vector2f yawvector;
	Matrix3f temp 	= dcm.get_dcm_matrix();

	yawvector.x 	= temp.a.x; // sin
	yawvector.y 	= temp.b.x;	// cos
	yawvector.normalize();

	cos_yaw_x 		= yawvector.y;	// 0 x = north
	sin_yaw_y 		= yawvector.x;	// 1 y

	sin_pitch_y 	= -temp.c.x;
	cos_pitch_x 	= sqrt(1 - (temp.c.x * temp.c.x));

	cos_roll_x 		= temp.c.z / cos_pitch_x;
	sin_roll_y 		= temp.c.y / cos_pitch_x;

	//Vector3f accel_filt	= imu.get_accel_filtered();
	//accels_rot 	= dcm.get_dcm_matrix() * imu.get_accel_filtered();
}

// updated at 10hz
static void update_alt()
{
	altitude_sensor = BARO;

	#if HIL_MODE == HIL_MODE_ATTITUDE
	current_loc.alt = g_gps->altitude - gps_base_alt;
	return;
	#else

	if(g.sonar_enabled){
		// filter out offset
		float scale;

		// read barometer
		baro_alt 			= read_barometer();

		if(baro_alt < 1000){
			scale = (sonar_alt - 400) / 200;
			scale = constrain(scale, 0, 1);
			current_loc.alt = ((float)sonar_alt * (1.0 - scale)) + ((float)baro_alt * scale) + home.alt;
		}else{
			current_loc.alt = baro_alt + home.alt;
		}

	}else{
		baro_alt 		= read_barometer();
		// no sonar altitude
		current_loc.alt = baro_alt + home.alt;
	}

	#endif
}

static void
adjust_altitude()
{
	flight_timer++;
	if(flight_timer >= 2){
		flight_timer = 0;

		if(g.rc_3.control_in <= 200){
			next_WP.alt -= 3;												// 1 meter per second
			next_WP.alt = max(next_WP.alt, (current_loc.alt - 900));		// don't go more than 4 meters below current location

		}else if (g.rc_3.control_in > 700){
			next_WP.alt += 4;												// 1 meter per second
			//next_WP.alt = min((current_loc.alt + 400), next_WP.alt);		// don't go more than 4 meters below current location
			next_WP.alt = min(next_WP.alt, (current_loc.alt + 600));		// don't go more than 4 meters below current location
		}
		next_WP.alt = max(next_WP.alt, 100);		// don't go more than 4 meters below current location
	}
}

static void tuning(){

	//Outer Loop : Attitude
	#if CHANNEL_6_TUNING == CH6_STABILIZE_KP
		g.pid_stabilize_roll.kP((float)g.rc_6.control_in / 1000.0);
		g.pid_stabilize_pitch.kP((float)g.rc_6.control_in / 1000.0);

	#elif CHANNEL_6_TUNING == CH6_STABILIZE_KI
		g.pid_stabilize_roll.kI((float)g.rc_6.control_in / 1000.0);
		g.pid_stabilize_pitch.kI((float)g.rc_6.control_in / 1000.0);

	#elif CHANNEL_6_TUNING == CH6_YAW_KP
		g.pid_stabilize_yaw.kP((float)g.rc_6.control_in / 1000.0);  // range from 0.0 ~ 5.0

	#elif CHANNEL_6_TUNING == CH6_YAW_KI
		g.pid_stabilize_yaw.kI((float)g.rc_6.control_in / 1000.0);


	//Inner Loop : Rate
	#elif CHANNEL_6_TUNING == CH6_RATE_KP
		g.pid_rate_roll.kP((float)g.rc_6.control_in / 1000.0);
		g.pid_rate_pitch.kP((float)g.rc_6.control_in / 1000.0);

	#elif CHANNEL_6_TUNING == CH6_RATE_KI
		g.pid_rate_roll.kI((float)g.rc_6.control_in / 1000.0);
		g.pid_rate_pitch.kI((float)g.rc_6.control_in / 1000.0);

	#elif CHANNEL_6_TUNING == CH6_YAW_RATE_KP
		g.pid_rate_yaw.kP((float)g.rc_6.control_in / 1000.0);

	#elif CHANNEL_6_TUNING == CH6_YAW_RATE_KI
		g.pid_rate_yaw.kI((float)g.rc_6.control_in / 1000.0);


	//Altitude Hold
	#elif CHANNEL_6_TUNING == CH6_THROTTLE_KP
		g.pid_throttle.kP((float)g.rc_6.control_in / 1000.0); //  0 to 1

	#elif CHANNEL_6_TUNING == CH6_THROTTLE_KD
		g.pid_throttle.kD((float)g.rc_6.control_in / 1000.0); //  0 to 1

	//Extras
	#elif CHANNEL_6_TUNING == CH6_TOP_BOTTOM_RATIO
		g.top_bottom_ratio = (float)g.rc_6.control_in / 1000.0;

	#elif CHANNEL_6_TUNING == CH6_PMAX
		g.pitch_max.set(g.rc_6.control_in * 2);  // 0 to 2000

        // Simple relay control
        #elif CHANNEL_6_TUNING == CH6_RELAY
              if(g.rc_6.control_in <= 600) relay_on();
              if(g.rc_6.control_in >= 400) relay_off();

	#endif


}

static void update_nav_wp()
{
	// XXX Guided mode!!!
	if(wp_control == LOITER_MODE){
		// calc a pitch to the target
		calc_loiter_nav();

		// rotate pitch and roll to the copter frame of reference
		calc_loiter_output();

	} else {
		// how far are we from the ideal trajectory?
		// this pushes us back on course
		update_crosstrack();

		// calc a rate dampened pitch to the target
		calc_rate_nav(g.waypoint_speed_max.get());

		// rotate that pitch to the copter frame of reference
		calc_nav_output();
	}
}

static void update_nav_yaw()
{
	// this tracks a location so the copter is always pointing towards it.
	if(yaw_tracking == MAV_ROI_LOCATION){
		nav_yaw = get_bearing(&current_loc, &target_WP);

	}else if(yaw_tracking == MAV_ROI_WPNEXT){
		nav_yaw = target_bearing;
	}
}

static void point_at_home_yaw()
{
	nav_yaw = get_bearing(&current_loc, &home);
}

static void auto_throttle()
{
	// get the AP throttle
	nav_throttle = get_nav_throttle(altitude_error);

	// apply throttle control
	//g.rc_3.servo_out = get_throttle(nav_throttle - throttle_slew);
	g.rc_3.servo_out = get_throttle(nav_throttle);

	//if(motor_armed){
		// remember throttle offset
		//throttle_slew = g.rc_3.servo_out - g.rc_3.control_in;
	//}else{
		// don't allow
		//throttle_slew = 0;
	//}

	// clear the new data flag
	invalid_throttle = false;

	//Serial.printf("wp:%d, \te:%d \tt%d \t%d\n", (int)next_WP.alt, (int)altitude_error, nav_throttle, g.rc_3.servo_out);
}