// -*- tab-width: 4; Mode: C++; c-basic-offset: 4; indent-tabs-mode: nil -*-
/*****************************************************************************
The init_ardupilot function processes everything we need for an in - air restart
	We will determine later if we are actually on the ground and process a
	ground start in that case.

*****************************************************************************/

#if CLI_ENABLED == ENABLED
// Functions called from the top-level menu
static int8_t	process_logs(uint8_t argc, const Menu::arg *argv);	// in Log.pde
static int8_t	setup_mode(uint8_t argc, const Menu::arg *argv);	// in setup.pde
static int8_t	test_mode(uint8_t argc, const Menu::arg *argv);		// in test.cpp
static int8_t	planner_mode(uint8_t argc, const Menu::arg *argv);	// in planner.pde

// This is the help function
// PSTR is an AVR macro to read strings from flash memory
// printf_P is a version of print_f that reads from flash memory
static int8_t	main_menu_help(uint8_t argc, const Menu::arg *argv)
{
	Serial.printf_P(PSTR("Commands:\n"
						 "  logs\n"
						 "  setup\n"
						 "  test\n"
 						 "  planner\n"
 						 "\n"
						 "Move the slide switch and reset to FLY.\n"
						 "\n"));
	return(0);
}

// Command/function table for the top-level menu.
const struct Menu::command main_menu_commands[] PROGMEM = {
//   command		function called
//   =======        ===============
	{"logs",		process_logs},
	{"setup",		setup_mode},
	{"test",		test_mode},
	{"help",		main_menu_help},
	{"planner",		planner_mode}
};

// Create the top-level menu object.
MENU(main_menu, THISFIRMWARE, main_menu_commands);

// the user wants the CLI. It never exits
static void run_cli(void)
{
    while (1) {
        main_menu.run();
    }
}

#endif // CLI_ENABLED

static void init_ardupilot()
{
	// Console serial port
	//
	// The console port buffers are defined to be sufficiently large to support
	// the console's use as a logging device, optionally as the GPS port when
	// GPS_PROTOCOL_IMU is selected, and as the telemetry port.
	//
	// XXX This could be optimised to reduce the buffer sizes in the cases
	// where they are not otherwise required.
	//
	Serial.begin(SERIAL0_BAUD, 128, 128);

	// GPS serial port.
	//
	// Not used if the IMU/X-Plane GPS is in use.
	//
	// XXX currently the EM406 (SiRF receiver) is nominally configured
	// at 57600, however it's not been supported to date.  We should
	// probably standardise on 38400.
	//
	// XXX the 128 byte receive buffer may be too small for NMEA, depending
	// on the message set configured.
	//
	#if GPS_PROTOCOL != GPS_PROTOCOL_IMU
	Serial1.begin(38400, 128, 16);
	#endif

	Serial.printf_P(PSTR("\n\nInit " THISFIRMWARE
						 "\n\nFree RAM: %u\n"),
                    memcheck_available_memory());


	//
	// Check the EEPROM format version before loading any parameters from EEPROM.
	//
	report_version();

	// setup IO pins
	pinMode(C_LED_PIN, OUTPUT);				// GPS status LED
	pinMode(A_LED_PIN, OUTPUT);				// GPS status LED
	pinMode(B_LED_PIN, OUTPUT);				// GPS status LED
	pinMode(SLIDE_SWITCH_PIN, INPUT);		// To enter interactive mode
	pinMode(PUSHBUTTON_PIN, INPUT);			// unused
	DDRL |= B00000100;						// Set Port L, pin 2 to output for the relay

	// XXX set Analog out 14 to output
	//  	   76543210
	//DDRK |= B01010000;

	#if MOTOR_LEDS == 1
		pinMode(FR_LED, OUTPUT);			// GPS status LED
		pinMode(RE_LED, OUTPUT);			// GPS status LED
		pinMode(RI_LED, OUTPUT);			// GPS status LED
		pinMode(LE_LED, OUTPUT);			// GPS status LED
	#endif

	#if PIEZO == 1
		pinMode(PIEZO_PIN,OUTPUT);
		piezo_beep();
	#endif


	if (!g.format_version.load() ||
	     g.format_version != Parameters::k_format_version) {
		//Serial.printf_P(PSTR("\n\nForcing complete parameter reset..."));

		/*Serial.printf_P(PSTR("\n\nEEPROM format version  %d not compatible with this firmware (requires %d)"
		                     "\n\nForcing complete parameter reset..."),
		                     g.format_version.get(),
		                     Parameters::k_format_version);
		*/

		// erase all parameters
		Serial.printf_P(PSTR("Firmware change: erasing EEPROM...\n"));
		delay(100); // wait for serial send
		AP_Var::erase_all();

		// save the new format version
		g.format_version.set_and_save(Parameters::k_format_version);

		// save default radio values
		default_dead_zones();

		Serial.printf_P(PSTR("Please Run Setup...\n"));
		while (true) {
			delay(1000);
			if(motor_light){
				digitalWrite(A_LED_PIN, HIGH);
				digitalWrite(B_LED_PIN, HIGH);
				digitalWrite(C_LED_PIN, HIGH);
			}else{
				digitalWrite(A_LED_PIN, LOW);
				digitalWrite(B_LED_PIN, LOW);
				digitalWrite(C_LED_PIN, LOW);
			}
			motor_light = !motor_light;
		}

	}else{
		// save default radio values
		//default_dead_zones();

	    // Load all auto-loaded EEPROM variables
	    AP_Var::load_all();
	}

	// Telemetry port.
	//
	// Not used if telemetry is going to the console.
	//
	// XXX for unidirectional protocols, we could (should) minimize
	// the receive buffer, and the transmit buffer could also be
	// shrunk for protocols that don't send large messages.
	//
	Serial3.begin(map_baudrate(g.serial3_baud,SERIAL3_BAUD), 128, 128);

	#ifdef RADIO_OVERRIDE_DEFAULTS
	{
		int16_t rc_override[8] = RADIO_OVERRIDE_DEFAULTS;
		APM_RC.setHIL(rc_override);
	}
	#endif

    #if FRAME_CONFIG ==	HELI_FRAME
		g.heli_servo_manual = false;
		heli_init_swash();  // heli initialisation
	#endif

	init_rc_in();		// sets up rc channels from radio
	init_rc_out();		// sets up the timer libs
	init_camera();

	#if HIL_MODE != HIL_MODE_ATTITUDE
		// begin filtering the ADC Gyros
		adc.filter_result = true;

		adc.Init();	 		// APM ADC library initialization
		barometer.Init();	// APM Abs Pressure sensor initialization
	#endif

	// Do GPS init
	g_gps = &g_gps_driver;
	g_gps->init();			// GPS Initialization
    g_gps->callback = mavlink_delay;

	// init the GCS
    gcs0.init(&Serial);
    gcs3.init(&Serial3);

	if(g.compass_enabled)
		init_compass();

	#ifdef OPTFLOW_ENABLED
	// init the optical flow sensor
	if(g.optflow_enabled) {
		init_optflow();
	}
	#endif

// agmatthews USERHOOKS
#ifdef USERHOOK_INIT
   USERHOOK_INIT
#endif
	// Logging:
	// --------
	// DataFlash log initialization
#if LOGGING_ENABLED == ENABLED
	DataFlash.Init();
#endif

#if CLI_ENABLED == ENABLED && CLI_SLIDER_ENABLED == ENABLED
	// If the switch is in 'menu' mode, run the main menu.
	//
	// Since we can't be sure that the setup or test mode won't leave
	// the system in an odd state, we don't let the user exit the top
	// menu; they must reset in order to fly.
	//
	if (check_startup_for_CLI()) {
		digitalWrite(A_LED_PIN,HIGH);		// turn on setup-mode LED
		Serial.printf_P(PSTR("\nCLI:\n\n"));
        run_cli();
	}
#else
    Serial.printf_P(PSTR("\nPress ENTER 3 times to start interactive setup\n\n"));
#endif // CLI_ENABLED

    if(g.esc_calibrate == 1){
        init_esc();
    }

	// Logging:
	// --------
	if(g.log_bitmask != 0){
		//	TODO - Here we will check  on the length of the last log
		//  We don't want to create a bunch of little logs due to powering on and off
		start_new_log();
	}

    GPS_enabled = false;

	#if HIL_MODE == HIL_MODE_DISABLED
    // Read in the GPS
	for (byte counter = 0; ; counter++) {
		g_gps->update();
		if (g_gps->status() != 0){
			GPS_enabled = true;
			break;
		}

		if (counter >= 2) {
			GPS_enabled = false;
			break;
	    }
	}
	#else
		GPS_enabled = true;
	#endif

	// lengthen the idle timeout for gps Auto_detect
	// ---------------------------------------------
	g_gps->idleTimeout = 20000;

	// print the GPS status
	// --------------------
	report_gps();

	#if HIL_MODE != HIL_MODE_ATTITUDE
	// read Baro pressure at ground
	//-----------------------------
	init_barometer();
	#endif

	// initialize commands
	// -------------------
	init_commands();

	// set the correct flight mode
	// ---------------------------
	reset_control_switch();

	#if HIL_MODE != HIL_MODE_ATTITUDE
		dcm.kp_roll_pitch(0.030000);
		dcm.ki_roll_pitch(0.00001278),	// 50 hz I term
		dcm.kp_yaw(0.08);
		dcm.ki_yaw(0.00004);
	#endif

	// init the Z damopener
	// --------------------
	#if ACCEL_ALT_HOLD == 1
	init_z_damper();
	#endif


	startup_ground();

	Log_Write_Startup();

	SendDebug("\nReady to FLY ");
}

//********************************************************************************
//This function does all the calibrations, etc. that we need during a ground start
//********************************************************************************
static void startup_ground(void)
{
	gcs_send_text_P(SEVERITY_LOW,PSTR("GROUND START"));

	#if HIL_MODE != HIL_MODE_ATTITUDE
		// Warm up and read Gyro offsets
		// -----------------------------
		imu.init_gyro(mavlink_delay);
		#if CLI_ENABLED == ENABLED
			report_imu();
		#endif
	#endif

	// reset the leds
	// ---------------------------
	clear_leds();
}

/*
#define YAW_HOLD 			0
#define YAW_ACRO 			1
#define YAW_AUTO 			2
#define YAW_LOOK_AT_HOME 	3

#define ROLL_PITCH_STABLE 	0
#define ROLL_PITCH_ACRO 	1
#define ROLL_PITCH_AUTO		2

#define THROTTLE_MANUAL 	0
#define THROTTLE_HOLD 		1
#define THROTTLE_AUTO		2

*/

static void set_mode(byte mode)
{
	if(control_mode == mode){
		// don't switch modes if we are already in the correct mode.
		return;
	}

	old_control_mode = control_mode;

	control_mode = mode;
	control_mode = constrain(control_mode, 0, NUM_MODES - 1);

	// used to stop fly_aways
	motor_auto_armed = (g.rc_3.control_in > 0);

	// clearing value used in interactive alt hold
	manual_boost = 0;

	// clearing value used to set WP's dynamically.
	CH7_wp_index = 0;

	Serial.println(flight_mode_strings[control_mode]);

	// report the GPS and Motor arming status
	led_mode = NORMAL_LEDS;

	switch(control_mode)
	{
		case ACRO:
			yaw_mode 		= YAW_ACRO;
			roll_pitch_mode = ROLL_PITCH_ACRO;
			throttle_mode 	= THROTTLE_MANUAL;
			break;

		case STABILIZE:
			yaw_mode 		= YAW_HOLD;
			roll_pitch_mode = ROLL_PITCH_STABLE;
			throttle_mode 	= THROTTLE_MANUAL;
			break;

		case ALT_HOLD:
			yaw_mode 		= ALT_HOLD_YAW;
			roll_pitch_mode = ALT_HOLD_RP;
			throttle_mode 	= ALT_HOLD_THR;

			next_WP = current_loc;
			break;

		case AUTO:
			yaw_mode 		= AUTO_YAW;
			roll_pitch_mode = AUTO_RP;
			throttle_mode 	= AUTO_THR;

			// loads the commands from where we left off
			init_commands();
			break;

		case CIRCLE:
			yaw_mode 		= CIRCLE_YAW;
			roll_pitch_mode = CIRCLE_RP;
			throttle_mode 	= CIRCLE_THR;

			next_WP 		= current_loc;
			break;

		case LOITER:
			yaw_mode 		= LOITER_YAW;
			roll_pitch_mode = LOITER_RP;
			throttle_mode 	= LOITER_THR;

			next_WP 		= current_loc;
			break;

		case POSITION:
			yaw_mode 		= YAW_HOLD;
			roll_pitch_mode = ROLL_PITCH_AUTO;
			throttle_mode 	= THROTTLE_MANUAL;

			next_WP 		= current_loc;
			break;

		case GUIDED:
			yaw_mode 		= YAW_AUTO;
			roll_pitch_mode = ROLL_PITCH_AUTO;
			throttle_mode 	= THROTTLE_AUTO;

			next_WP = current_loc;
			set_next_WP(&guided_WP);
			break;

		case RTL:
			yaw_mode 		= RTL_YAW;
			roll_pitch_mode = RTL_RP;
			throttle_mode 	= RTL_THR;

			do_RTL();
			break;

		default:
			break;
	}

	if(throttle_mode == THROTTLE_MANUAL){
		// reset all of the throttle iterms
		g.pi_alt_hold.reset_I();
		g.pi_throttle.reset_I();
	}else { // an automatic throttle

		// todo: replace with a throttle cruise estimator
		init_throttle_cruise();
	}

	if(roll_pitch_mode <= ROLL_PITCH_ACRO){
		// We are under manual attitude control
		// reset out nav parameters
		reset_nav();
	}

	Log_Write_Mode(control_mode);
}

static void set_failsafe(boolean mode)
{
	// only act on changes
	// -------------------
	if(failsafe != mode){

		// store the value so we don't trip the gate twice
		// -----------------------------------------------
		failsafe = mode;

		if (failsafe == false){
			// We've regained radio contact
			// ----------------------------
			failsafe_off_event();

		}else{
			// We've lost radio contact
			// ------------------------
			failsafe_on_event();

		}
	}
}


static void
init_compass()
{
	compass.set_orientation(MAG_ORIENTATION);						// set compass's orientation on aircraft
	dcm.set_compass(&compass);
	compass.init();
	compass.get_offsets();					// load offsets to account for airframe magnetic interference
}

#ifdef OPTFLOW_ENABLED
static void
init_optflow()
{
	if( optflow.init() == false ) {
	    g.optflow_enabled = false;
	    //SendDebug("\nFailed to Init OptFlow ");
	}
	optflow.set_orientation(OPTFLOW_ORIENTATION);			// set optical flow sensor's orientation on aircraft
	optflow.set_field_of_view(OPTFLOW_FOV);					// set optical flow sensor's field of view
}
#endif

static void
init_simple_bearing()
{
	initial_simple_bearing = dcm.yaw_sensor;
}

static void
init_throttle_cruise()
{
	// are we moving from manual throttle to auto_throttle?
	if((old_control_mode <= STABILIZE) && (g.rc_3.control_in > MINIMUM_THROTTLE)){
		g.pi_throttle.reset_I();
		g.pi_alt_hold.reset_I();
		g.throttle_cruise.set_and_save(g.rc_3.control_in);
	}
}

#if CLI_ENABLED == ENABLED
#if BROKEN_SLIDER == 1

static boolean
check_startup_for_CLI()
{
	//return true;
	if((g.rc_4.radio_max) < 1600){
		// CLI mode
		return true;

	}else if(abs(g.rc_4.control_in) > 3000){
		// CLI mode
		return true;

	}else{
		// startup to fly
		return false;
	}
}

#else

static boolean
check_startup_for_CLI()
{
	return (digitalRead(SLIDE_SWITCH_PIN) == 0);
}

#endif // BROKEN_SLIDER
#endif // CLI_ENABLED

/*
  map from a 8 bit EEPROM baud rate to a real baud rate
 */
static uint32_t map_baudrate(int8_t rate, uint32_t default_baud)
{
    switch (rate) {
    case 9:    return 9600;
    case 19:   return 19200;
    case 38:   return 38400;
    case 57:   return 57600;
    case 111:  return 111100;
    case 115:  return 115200;
    }
    //Serial.println_P(PSTR("Invalid SERIAL3_BAUD"));
    return default_baud;
}