ardupilot/ArduCopter/test.pde

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

#if CLI_ENABLED == ENABLED

// These are function definitions so the Menu can be constructed before the functions
// are defined below. Order matters to the compiler.
static int8_t	test_radio_pwm(uint8_t argc, 	const Menu::arg *argv);
static int8_t	test_radio(uint8_t argc, 		const Menu::arg *argv);
//static int8_t	test_failsafe(uint8_t argc, 	const Menu::arg *argv);
//static int8_t	test_stabilize(uint8_t argc, 	const Menu::arg *argv);
static int8_t	test_gps(uint8_t argc, 			const Menu::arg *argv);
//static int8_t	test_tri(uint8_t argc, 			const Menu::arg *argv);
//static int8_t	test_adc(uint8_t argc, 			const Menu::arg *argv);
static int8_t	test_ins(uint8_t argc, 			const Menu::arg *argv);
static int8_t	test_imu(uint8_t argc, 			const Menu::arg *argv);
//static int8_t	test_dcm_eulers(uint8_t argc, 	const Menu::arg *argv);
//static int8_t	test_dcm(uint8_t argc, 			const Menu::arg *argv);
//static int8_t	test_omega(uint8_t argc, 		const Menu::arg *argv);
//static int8_t	test_stab_d(uint8_t argc, 		const Menu::arg *argv);
static int8_t	test_battery(uint8_t argc, 		const Menu::arg *argv);
//static int8_t	test_boost(uint8_t argc, 		const Menu::arg *argv);
//static int8_t	test_wp_nav(uint8_t argc, 		const Menu::arg *argv);
//static int8_t	test_reverse(uint8_t argc, 		const Menu::arg *argv);
static int8_t	test_tuning(uint8_t argc, 		const Menu::arg *argv);
static int8_t	test_relay(uint8_t argc,	 	const Menu::arg *argv);
static int8_t	test_wp(uint8_t argc, 			const Menu::arg *argv);
#if HIL_MODE != HIL_MODE_ATTITUDE
static int8_t	test_baro(uint8_t argc, 		const Menu::arg *argv);
static int8_t	test_sonar(uint8_t argc, 		const Menu::arg *argv);
#endif
static int8_t	test_mag(uint8_t argc, 			const Menu::arg *argv);
static int8_t	test_optflow(uint8_t argc, 		const Menu::arg *argv);
static int8_t	test_logging(uint8_t argc, 		const Menu::arg *argv);
//static int8_t	test_xbee(uint8_t argc, 		const Menu::arg *argv);
static int8_t	test_eedump(uint8_t argc, 		const Menu::arg *argv);
static int8_t	test_rawgps(uint8_t argc, 		const Menu::arg *argv);
//static int8_t	test_mission(uint8_t argc, 		const Menu::arg *argv);

// this is declared here to remove compiler errors
extern void		print_latlon(BetterStream *s, int32_t lat_or_lon);	// in Log.pde

// This is the help function
// PSTR is an AVR macro to read strings from flash memory
// printf_P is a version of printf that reads from flash memory
/*static int8_t	help_test(uint8_t argc, 			const Menu::arg *argv)
{
	Serial.printf_P(PSTR("\n"
						 "Commands:\n"
						 "  radio\n"
						 "  servos\n"
						 "  g_gps\n"
						 "  imu\n"
						 "  battery\n"
						 "\n"));
}*/

// Creates a constant array of structs representing menu options
// and stores them in Flash memory, not RAM.
// User enters the string in the console to call the functions on the right.
// See class Menu in AP_Coommon for implementation details
const struct Menu::command test_menu_commands[] PROGMEM = {
	{"pwm",			test_radio_pwm},
	{"radio",		test_radio},
//	{"failsafe",	test_failsafe},
//	{"stabilize",	test_stabilize},
	{"gps",			test_gps},
//	{"adc", 		test_adc},
	{"ins", 		test_ins},
	{"imu",			test_imu},
//	{"dcm",			test_dcm_eulers},
	//{"omega",		test_omega},
//	{"stab_d",		test_stab_d},
	{"battery",		test_battery},
	{"tune",		test_tuning},
	//{"tri",			test_tri},
	{"relay",		test_relay},
	{"wp",			test_wp},
//	{"boost",		test_boost},
#if HIL_MODE != HIL_MODE_ATTITUDE
	{"altitude",	test_baro},
	{"sonar",		test_sonar},
#endif
	{"compass",		test_mag},
	{"optflow",		test_optflow},
	//{"xbee",		test_xbee},
	{"eedump",		test_eedump},
	{"logging",		test_logging},
//	{"rawgps",		test_rawgps},
//	{"mission",		test_mission},
	//{"reverse",		test_reverse},
	//{"wp",			test_wp_nav},
};

// A Macro to create the Menu
MENU(test_menu, "test", test_menu_commands);

static int8_t
test_mode(uint8_t argc, const Menu::arg *argv)
{
	//Serial.printf_P(PSTR("Test Mode\n\n"));
	test_menu.run();
	return 0;
}

static int8_t
test_eedump(uint8_t argc, const Menu::arg *argv)
{
	int		i, j;

	// hexdump the EEPROM
	for (i = 0; i < EEPROM_MAX_ADDR; i += 16) {
		Serial.printf_P(PSTR("%04x:"), i);
		for (j = 0; j < 16; j++)
			Serial.printf_P(PSTR(" %02x"), eeprom_read_byte((const uint8_t *)(i + j)));
		Serial.println();
	}
	return(0);
}


static int8_t
test_radio_pwm(uint8_t argc, const Menu::arg *argv)
{
	#if defined( __AVR_ATmega1280__ )  // test disabled to save code size for 1280
		print_test_disabled();
		return (0);
	#else
		print_hit_enter();
		delay(1000);

		while(1){
			delay(20);

			// Filters radio input - adjust filters in the radio.pde file
			// ----------------------------------------------------------
			read_radio();

			// servo Yaw
			//APM_RC.OutputCh(CH_7, g.rc_4.radio_out);

			Serial.printf_P(PSTR("IN: 1: %d\t2: %d\t3: %d\t4: %d\t5: %d\t6: %d\t7: %d\t8: %d\n"),
								g.rc_1.radio_in,
								g.rc_2.radio_in,
								g.rc_3.radio_in,
								g.rc_4.radio_in,
								g.rc_5.radio_in,
								g.rc_6.radio_in,
								g.rc_7.radio_in,
								g.rc_8.radio_in);

			if(Serial.available() > 0){
				return (0);
			}
		}
	#endif
}

/*
//static int8_t
//test_tri(uint8_t argc, const Menu::arg *argv)
{
	print_hit_enter();
	delay(1000);

	while(1){
		delay(20);

		// Filters radio input - adjust filters in the radio.pde file
		// ----------------------------------------------------------
		read_radio();
		g.rc_4.servo_out = g.rc_4.control_in;
		g.rc_4.calc_pwm();

		Serial.printf_P(PSTR("input: %d\toutput%d\n"),
							g.rc_4.control_in,
							g.rc_4.radio_out);

		APM_RC.OutputCh(CH_TRI_YAW, g.rc_4.radio_out);

		if(Serial.available() > 0){
			return (0);
		}
	}
}*/

/*
static int8_t
//test_boost(uint8_t argc, const Menu::arg *argv)
{
	print_hit_enter();
	delay(1000);
	int16_t temp = g.throttle_min;

	while(1){
		delay(20);
		g.rc_3.control_in = temp;
		adjust_altitude();
		Serial.printf("tmp:%d, boost: %d\n", temp, manual_boost);
		temp++;

		if(temp > MAXIMUM_THROTTLE){
			return (0);
		}
	}
}
//*/

static int8_t
test_radio(uint8_t argc, const Menu::arg *argv)
{
	print_hit_enter();
	delay(1000);

	while(1){
		delay(20);
		read_radio();


		Serial.printf_P(PSTR("IN  1: %d\t2: %d\t3: %d\t4: %d\t5: %d\t6: %d\t7: %d\n"),
							g.rc_1.control_in,
							g.rc_2.control_in,
							g.rc_3.control_in,
							g.rc_4.control_in,
							g.rc_5.control_in,
							g.rc_6.control_in,
							g.rc_7.control_in);

		//Serial.printf_P(PSTR("OUT 1: %d\t2: %d\t3: %d\t4: %d\n"), (g.rc_1.servo_out / 100), (g.rc_2.servo_out / 100), g.rc_3.servo_out, (g.rc_4.servo_out / 100));

		/*Serial.printf_P(PSTR(	"min: %d"
								"\t in: %d"
								"\t pwm_in: %d"
								"\t sout: %d"
								"\t pwm_out %d\n"),
								g.rc_3.radio_min,
								g.rc_3.control_in,
								g.rc_3.radio_in,
								g.rc_3.servo_out,
								g.rc_3.pwm_out
								);
		*/
		if(Serial.available() > 0){
			return (0);
		}
	}
}

/*
//static int8_t
//test_failsafe(uint8_t argc, const Menu::arg *argv)
{

	#if THROTTLE_FAILSAFE
	byte fail_test;
	print_hit_enter();
	for(int i = 0; i < 50; i++){
		delay(20);
		read_radio();
	}

	oldSwitchPosition = readSwitch();

	Serial.printf_P(PSTR("Unplug battery, throttle in neutral, turn off radio.\n"));
	while(g.rc_3.control_in > 0){
		delay(20);
		read_radio();
	}

	while(1){
		delay(20);
		read_radio();

		if(g.rc_3.control_in > 0){
			Serial.printf_P(PSTR("THROTTLE CHANGED %d \n"), g.rc_3.control_in);
			fail_test++;
		}

		if(oldSwitchPosition != readSwitch()){
			Serial.printf_P(PSTR("CONTROL MODE CHANGED: "));
			Serial.println(flight_mode_strings[readSwitch()]);
			fail_test++;
		}

		if(g.throttle_fs_enabled && g.rc_3.get_failsafe()){
			Serial.printf_P(PSTR("THROTTLE FAILSAFE ACTIVATED: %d, "), g.rc_3.radio_in);
			Serial.println(flight_mode_strings[readSwitch()]);
			fail_test++;
		}

		if(fail_test > 0){
			return (0);
		}
		if(Serial.available() > 0){
			Serial.printf_P(PSTR("LOS caused no change in ACM.\n"));
			return (0);
		}
	}
	#else
		return (0);
	#endif
}
*/

/*
//static int8_t
//test_stabilize(uint8_t argc, const Menu::arg *argv)
{
	static byte ts_num;


	print_hit_enter();
	delay(1000);

	// setup the radio
	// ---------------
	init_rc_in();

	control_mode = STABILIZE;
	Serial.printf_P(PSTR("g.pi_stabilize_roll.kP: %4.4f\n"), g.pi_stabilize_roll.kP());
	Serial.printf_P(PSTR("max_stabilize_dampener:%d\n\n "), max_stabilize_dampener);

	motors.auto_armed(false);
	motors.armed(true);

	while(1){
		// 50 hz
		if (millis() - fast_loopTimer > 19) {
			delta_ms_fast_loop 	= millis() - fast_loopTimer;
			fast_loopTimer		= millis();
			G_Dt 				= (float)delta_ms_fast_loop / 1000.f;

			if(g.compass_enabled){
				medium_loopCounter++;
				if(medium_loopCounter == 5){
                    Matrix3f m = dcm.get_dcm_matrix();
					compass.read();		 				// Read magnetometer
                    compass.null_offsets();
					medium_loopCounter = 0;
				}
			}

			// for trim features
			read_trim_switch();

			// Filters radio input - adjust filters in the radio.pde file
			// ----------------------------------------------------------
			read_radio();

			// IMU
			// ---
			read_AHRS();

			// allow us to zero out sensors with control switches
			if(g.rc_5.control_in < 600){
				dcm.roll_sensor = dcm.pitch_sensor = 0;
			}

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

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

			ts_num++;
			if (ts_num > 10){
				ts_num = 0;
				Serial.printf_P(PSTR("r: %d, p:%d, rc1:%d, "),
					(int)(dcm.roll_sensor/100),
					(int)(dcm.pitch_sensor/100),
					g.rc_1.pwm_out);

				print_motor_out();
			}
			// R: 1417,  L: 1453  F: 1453  B: 1417

			//Serial.printf_P(PSTR("timer: %d, r: %d\tp: %d\t y: %d\n"), (int)delta_ms_fast_loop, ((int)dcm.roll_sensor/100), ((int)dcm.pitch_sensor/100), ((uint16_t)dcm.yaw_sensor/100));
			//Serial.printf_P(PSTR("timer: %d, r: %d\tp: %d\t y: %d\n"), (int)delta_ms_fast_loop, ((int)dcm.roll_sensor/100), ((int)dcm.pitch_sensor/100), ((uint16_t)dcm.yaw_sensor/100));

			if(Serial.available() > 0){
				if(g.compass_enabled){
					compass.save_offsets();
					report_compass();
				}
				return (0);
			}

		}
	}
}
*/


/*
#if HIL_MODE != HIL_MODE_ATTITUDE && CONFIG_ADC == ENABLED
//static int8_t
//test_adc(uint8_t argc, const Menu::arg *argv)
{
	print_hit_enter();
	Serial.printf_P(PSTR("ADC\n"));
	delay(1000);

  adc.Init(&timer_scheduler);

  delay(50);

	while(1){
		for(int i = 0; i < 9; i++){
			Serial.printf_P(PSTR("%.1f,"),adc.Ch(i));
		}
		Serial.println();
		delay(20);
		if(Serial.available() > 0){
			return (0);
		}
	}
}
#endif
*/

static int8_t
test_ins(uint8_t argc, const Menu::arg *argv)
{
	#if defined( __AVR_ATmega1280__ )  // test disabled to save code size for 1280
		print_test_disabled();
		return (0);
	#else
		float gyro[3], accel[3], temp;
		print_hit_enter();
		Serial.printf_P(PSTR("InertialSensor\n"));
		delay(1000);

		ins.init(&timer_scheduler);

		delay(50);

		while(1){
			ins.update();
			ins.get_gyros(gyro);
			ins.get_accels(accel);
			temp = ins.temperature();

			Serial.printf_P(PSTR("g"));

			for (int i = 0; i < 3; i++) {
				Serial.printf_P(PSTR(" %7.4f"), gyro[i]);
			}

			Serial.printf_P(PSTR(" a"));

			for (int i = 0; i < 3; i++) {
				Serial.printf_P(PSTR(" %7.4f"),accel[i]);
			}
			Serial.printf_P(PSTR(" t %7.4f \n"), temp);
			delay(40);
			if(Serial.available() > 0){
				return (0);
			}
		}
	#endif
}


/*
  test the IMU interface
 */
static int8_t
test_imu(uint8_t argc, const Menu::arg *argv)
{
	#if defined( __AVR_ATmega1280__ )  // test disabled to save code size for 1280
		print_test_disabled();
		return (0);
	#else
		Vector3f gyro;
		Vector3f accel;

		imu.init(IMU::WARM_START, delay, flash_leds, &timer_scheduler);

		report_imu();
		imu.init_gyro(delay, flash_leds);
		report_imu();

		print_hit_enter();
		delay(1000);

		while(1){
			delay(40);

			imu.update();
			gyro = imu.get_gyro();
			accel = imu.get_accel();

			Serial.printf_P(PSTR("g %8.4f %8.4f %8.4f"), gyro.x, gyro.y, gyro.z);
			Serial.printf_P(PSTR("  a %8.4f %8.4f %8.4f\n"), accel.x, accel.y, accel.z);

			if(Serial.available() > 0){
				return (0);
			}
		}
	#endif
}


/*
   test the DCM code, printing Euler angles
 */
/*static int8_t
//test_dcm_eulers(uint8_t argc, const Menu::arg *argv)
{

	//Serial.printf_P(PSTR("Calibrating."));

	//dcm.kp_yaw(0.02);
	//dcm.ki_yaw(0);

	imu.init(IMU::WARM_START, delay, flash_leds, &timer_scheduler);

	report_imu();
	imu.init_gyro(delay, flash_leds);
	report_imu();

	print_hit_enter();
	delay(1000);

	//float cos_roll, sin_roll, cos_pitch, sin_pitch, cos_yaw, sin_yaw;
	fast_loopTimer = millis();

	while(1){
		//delay(20);
		if (millis() - fast_loopTimer >=20) {

			// IMU
			// ---
			read_AHRS();
			medium_loopCounter++;

			if(medium_loopCounter == 4){
				update_trig();
			}

			if(medium_loopCounter == 1){
				medium_loopCounter = 0;
				Serial.printf_P(PSTR("dcm: %6.1f, %6.1f, %6.1f   omega: %6.1f, %6.1f, %6.1f\n"),
								dcm.roll_sensor/100.0,
								dcm.pitch_sensor/100.0,
								dcm.yaw_sensor/100.0,
								degrees(omega.x),
								degrees(omega.y),
								degrees(omega.z));

				if(g.compass_enabled){
					compass.read();		 				// Read magnetometer
                    compass.null_offsets();
				}
			}
			fast_loopTimer = millis();
		}
		if(Serial.available() > 0){
			return (0);
		}
	}
	return (0);
}*/

static int8_t
test_gps(uint8_t argc, const Menu::arg *argv)
{
    // test disabled to save code size for 1280
	#if defined( __AVR_ATmega1280__ ) || HIL_MODE != HIL_MODE_DISABLED
		print_test_disabled();
		return (0);
	#else
		print_hit_enter();
		delay(1000);

		while(1){
			delay(333);

			// Blink GPS LED if we don't have a fix
			// ------------------------------------
			update_GPS_light();

			g_gps->update();

			if (g_gps->new_data){
				Serial.printf_P(PSTR("Lat: "));
				print_latlon(&Serial, g_gps->latitude);
				Serial.printf_P(PSTR(", Lon "));
				print_latlon(&Serial, g_gps->longitude);
				Serial.printf_P(PSTR(", Alt: %ldm, #sats: %d\n"),
						g_gps->altitude/100,
						g_gps->num_sats);
				g_gps->new_data = false;
			}else{
				Serial.print(".");
			}
			if(Serial.available() > 0){
				return (0);
			}
		}
		return 0;
	#endif
}

// used to test the gain scheduler for Stab_D
/*
static int8_t
test_stab_d(uint8_t argc, const Menu::arg *argv)
{
	int16_t i = 0;
	g.stabilize_d = 1;

	g.stabilize_d_schedule = 1
	for (i = -4600; i < 4600; i+=10) {
		new_radio_frame = true;
		g.rc_1.control_in = i;
		g.rc_2.control_in = i;
		update_roll_pitch_mode();
    	Serial.printf("rin:%d, d:%1.6f \tpin:%d, d:%1.6f\n",g.rc_1.control_in, roll_scale_d, g.rc_2.control_in, pitch_scale_d);
    }
	g.stabilize_d_schedule = .5
	for (i = -4600; i < 4600; i+=10) {
		new_radio_frame = true;
		g.rc_1.control_in = i;
		g.rc_2.control_in = i;
		update_roll_pitch_mode();
    	Serial.printf("rin:%d, d:%1.6f \tpin:%d, d:%1.6f\n",g.rc_1.control_in, roll_scale_d, g.rc_2.control_in, pitch_scale_d);
    }

	g.stabilize_d_schedule = 0
	for (i = -4600; i < 4600; i+=10) {
		new_radio_frame = true;
		g.rc_1.control_in = i;
		g.rc_2.control_in = i;
		update_roll_pitch_mode();
    	Serial.printf("rin:%d, d:%1.6f \tpin:%d, d:%1.6f\n",g.rc_1.control_in, roll_scale_d, g.rc_2.control_in, pitch_scale_d);
    }

}*/

/*
//static int8_t
//test_dcm(uint8_t argc, const Menu::arg *argv)
{
	print_hit_enter();
	delay(1000);
	Serial.printf_P(PSTR("Gyro | Accel\n"));
	Vector3f 	_cam_vector;
	Vector3f 	_out_vector;

	G_Dt = .02;

	while(1){
		for(byte i = 0; i <= 50; i++){
			delay(20);
			// IMU
			// ---
			read_AHRS();
		}

		Matrix3f temp = dcm.get_dcm_matrix();
		Matrix3f temp_t = dcm.get_dcm_transposed();

		Serial.printf_P(PSTR("dcm\n"
							 "%4.4f \t %4.4f \t %4.4f \n"
							 "%4.4f \t %4.4f \t %4.4f \n"
							 "%4.4f \t %4.4f \t %4.4f \n\n"),
							temp.a.x, temp.a.y, temp.a.z,
							temp.b.x, temp.b.y, temp.b.z,
							temp.c.x, temp.c.y, temp.c.z);

		int _pitch 		= degrees(-asin(temp.c.x));
		int _roll 		= degrees(atan2(temp.c.y, temp.c.z));
		int _yaw 		= degrees(atan2(temp.b.x, temp.a.x));
		Serial.printf_P(PSTR(	"angles\n"
								"%d \t %d \t %d\n\n"),
								_pitch,
								_roll,
								_yaw);

		//_out_vector = _cam_vector * temp;
		//Serial.printf_P(PSTR(	"cam\n"
		//						"%d \t %d \t %d\n\n"),
		//						(int)temp.a.x * 100, (int)temp.a.y * 100, (int)temp.a.x * 100);

		if(Serial.available() > 0){
			return (0);
		}
	}
}
*/
/*
//static int8_t
//test_dcm(uint8_t argc, const Menu::arg *argv)
{
	print_hit_enter();
	delay(1000);
	Serial.printf_P(PSTR("Gyro | Accel\n"));
	delay(1000);

	while(1){
		Vector3f accels = dcm.get_accel();
		Serial.print("accels.z:");
		Serial.print(accels.z);
		Serial.print("omega.z:");
		Serial.print(omega.z);
		delay(100);

		if(Serial.available() > 0){
			return (0);
		}
	}
}
*/

/*static int8_t
//test_omega(uint8_t argc, const Menu::arg *argv)
{
	static byte ts_num;
	float old_yaw;

	print_hit_enter();
	delay(1000);
	Serial.printf_P(PSTR("Omega"));
	delay(1000);

	G_Dt = .02;

	while(1){
		delay(20);
		// IMU
		// ---
		read_AHRS();

		float my_oz = (dcm.yaw - old_yaw) * 50;

		old_yaw = dcm.yaw;

		ts_num++;
		if (ts_num > 2){
			ts_num = 0;
			//Serial.printf_P(PSTR("R: %4.4f\tP: %4.4f\tY: %4.4f\tY: %4.4f\n"), omega.x, omega.y, omega.z, my_oz);
			Serial.printf_P(PSTR(" Yaw: %ld\tY: %4.4f\tY: %4.4f\n"), dcm.yaw_sensor, omega.z, my_oz);
		}

		if(Serial.available() > 0){
			return (0);
		}
	}
	return (0);
}
//*/

static int8_t
test_tuning(uint8_t argc, const Menu::arg *argv)
{
	print_hit_enter();

	while(1){
		delay(200);
		read_radio();
		tuning();
		Serial.printf_P(PSTR("tune: %1.3f\n"), tuning_value);

		if(Serial.available() > 0){
			return (0);
		}
	}
}

static int8_t
test_battery(uint8_t argc, const Menu::arg *argv)
{
	#if defined( __AVR_ATmega1280__ )  // disable this test if we are using 1280
		print_test_disabled();
		return (0);
	#else
		Serial.printf_P(PSTR("\nCareful! Motors will spin! Press Enter to start.\n"));
		Serial.flush();
		while(!Serial.available()){
			delay(100);
		}
		Serial.flush();
		print_hit_enter();

		// allow motors to spin
		motors.enable();
		motors.armed(true);

		while(1){
			delay(100);
			read_radio();
			read_battery();
			if (g.battery_monitoring == 3){
				Serial.printf_P(PSTR("V: %4.4f\n"),
									battery_voltage1,
									current_amps1,
									current_total1);
			} else {
				Serial.printf_P(PSTR("V: %4.4f, A: %4.4f, Ah: %4.4f\n"),
									battery_voltage1,
									current_amps1,
									current_total1);
			}
			motors.throttle_pass_through();

			if(Serial.available() > 0){
				motors.armed(false);
				return (0);
			}
		}
		motors.armed(false);
		return (0);
	#endif
}

static int8_t test_relay(uint8_t argc, const Menu::arg *argv)
{
	#if defined( __AVR_ATmega1280__ )  // test disabled to save code size for 1280
		print_test_disabled();
		return (0);
	#else

		print_hit_enter();
		delay(1000);

		while(1){
			Serial.printf_P(PSTR("Relay on\n"));
			relay.on();
			delay(3000);
			if(Serial.available() > 0){
				return (0);
			}

			Serial.printf_P(PSTR("Relay off\n"));
			relay.off();
			delay(3000);
			if(Serial.available() > 0){
				return (0);
			}
		}
	#endif
}


static int8_t
test_wp(uint8_t argc, const Menu::arg *argv)
{
	delay(1000);

	// save the alitude above home option
	Serial.printf_P(PSTR("Hold alt "));
	if(g.RTL_altitude < 0){
		Serial.printf_P(PSTR("\n"));
	}else{
		Serial.printf_P(PSTR("of %dm\n"), (int)g.RTL_altitude / 100);
	}

	Serial.printf_P(PSTR("%d wp\n"), (int)g.command_total);
	Serial.printf_P(PSTR("Hit rad: %dm\n"), (int)g.waypoint_radius);
	//Serial.printf_P(PSTR("Loiter radius: %d\n\n"), (int)g.loiter_radius);

	report_wp();

	return (0);
}

//static int8_t test_rawgps(uint8_t argc, const Menu::arg *argv) {
	/*
   print_hit_enter();
   delay(1000);
	while(1){
		   if (Serial3.available()){
				   digitalWrite(B_LED_PIN, LED_ON); // Blink Yellow LED if we are sending data to GPS
				   Serial1.write(Serial3.read());
				   digitalWrite(B_LED_PIN, LED_OFF);
		   }
		   if (Serial1.available()){
				   digitalWrite(C_LED_PIN, LED_ON); // Blink Red LED if we are receiving data from GPS
				   Serial3.write(Serial1.read());
				   digitalWrite(C_LED_PIN, LED_OFF);
		   }
		   if(Serial.available() > 0){
				   return (0);
	 }
   }
   */
 //}

/*static int8_t
//test_xbee(uint8_t argc, const Menu::arg *argv)
{
	print_hit_enter();
	delay(1000);
	Serial.printf_P(PSTR("Begin XBee X-CTU Range and RSSI Test:\n"));

	while(1){
  		if (Serial3.available())
   			Serial3.write(Serial3.read());

		if(Serial.available() > 0){
			return (0);
		}
	}
}
*/

#if HIL_MODE != HIL_MODE_ATTITUDE
static int8_t
test_baro(uint8_t argc, const Menu::arg *argv)
{
	#if defined( __AVR_ATmega1280__ )  // test disabled to save code size for 1280
		print_test_disabled();
		return (0);
	#else
		print_hit_enter();
		init_barometer();

		while(1){
			delay(100);
			int32_t alt = read_barometer(); // calls barometer.read()

			int32_t pres = barometer.get_pressure();
			int16_t temp = barometer.get_temperature();
			int32_t raw_pres = barometer.get_raw_pressure();
			int32_t raw_temp = barometer.get_raw_temp();
			Serial.printf_P(PSTR("alt: %ldcm, pres: %ldmbar, temp: %d/100degC,"
								 " raw pres: %ld, raw temp: %ld\n"),
								 alt, pres ,temp, raw_pres, raw_temp);
			if(Serial.available() > 0){
				return (0);
			}
		}
		return 0;
	#endif
}
#endif


static int8_t
test_mag(uint8_t argc, const Menu::arg *argv)
{
	#if defined( __AVR_ATmega1280__ )  // test disabled to save code size for 1280
		print_test_disabled();
		return (0);
	#else
		if(g.compass_enabled) {
			print_hit_enter();

			while(1){
				delay(100);
				if (compass.read()) {
					float heading = compass.calculate_heading(ahrs.get_dcm_matrix());
					Vector3f maggy = compass.get_offsets();
					Serial.printf_P(PSTR("Heading: %ld, XYZ: %d, %d, %d\n"),
									(wrap_360(ToDeg(heading) * 100)) /100,
									compass.mag_x,
									compass.mag_y,
									compass.mag_z);
				} else {
					Serial.println_P(PSTR("not healthy"));
				}

				if(Serial.available() > 0){
					return (0);
				}
			}
		} else {
			Serial.printf_P(PSTR("Compass: "));
			print_enabled(false);
			return (0);
		}
		return (0);
	#endif
}

/*
//static int8_t
//test_reverse(uint8_t argc, 		const Menu::arg *argv)
{
	print_hit_enter();
	delay(1000);

	while(1){
		delay(20);

		// Filters radio input - adjust filters in the radio.pde file
		// ----------------------------------------------------------
		g.rc_4.set_reverse(0);
		g.rc_4.set_pwm(APM_RC.InputCh(CH_4));
		g.rc_4.servo_out = g.rc_4.control_in;
		g.rc_4.calc_pwm();
		Serial.printf_P(PSTR("PWM:%d input: %d\toutput%d "),
							APM_RC.InputCh(CH_4),
							g.rc_4.control_in,
							g.rc_4.radio_out);
		APM_RC.OutputCh(CH_6, g.rc_4.radio_out);


		g.rc_4.set_reverse(1);
		g.rc_4.set_pwm(APM_RC.InputCh(CH_4));
		g.rc_4.servo_out = g.rc_4.control_in;
		g.rc_4.calc_pwm();
		Serial.printf_P(PSTR("\trev input: %d\toutput%d\n"),
							g.rc_4.control_in,
							g.rc_4.radio_out);

		APM_RC.OutputCh(CH_7, g.rc_4.radio_out);

		if(Serial.available() > 0){
			g.rc_4.set_reverse(0);
			return (0);
		}
	}
}*/

#if HIL_MODE != HIL_MODE_ATTITUDE
/*
  test the sonar
 */
static int8_t
test_sonar(uint8_t argc, const Menu::arg *argv)
{
	if(g.sonar_enabled == false){
		Serial.printf_P(PSTR("Sonar disabled\n"));
		return (0);
	}

	// make sure sonar is initialised
	init_sonar();

	print_hit_enter();
	while(1) {
		delay(100);

		Serial.printf_P(PSTR("Sonar: %d cm\n"), sonar.read());
		//Serial.printf_P(PSTR("Sonar, %d, %d\n"), sonar.read(), sonar.raw_value);

		if(Serial.available() > 0){
			return (0);
		}
	}

	return (0);
}
#endif


static int8_t
test_optflow(uint8_t argc, const Menu::arg *argv)
{
	#ifdef OPTFLOW_ENABLED
	if(g.optflow_enabled) {
		Serial.printf_P(PSTR("man id: %d\t"),optflow.read_register(ADNS3080_PRODUCT_ID));
		print_hit_enter();

		while(1){
			delay(200);
			optflow.update();
			Log_Write_Optflow();
			Serial.printf_P(PSTR("x/dx: %d/%d\t y/dy %d/%d\t squal:%d\n"),
						optflow.x,
						optflow.dx,
						optflow.y,
						optflow.dy,
						optflow.surface_quality);

			if(Serial.available() > 0){
				return (0);
			}
		}
	} else {
		Serial.printf_P(PSTR("OptFlow: "));
		print_enabled(false);
	}
	return (0);

	#else
		print_test_disabled();
		return (0);
	#endif
}


/*
  test the dataflash is working
 */

static int8_t
test_logging(uint8_t argc, const Menu::arg *argv)
{
	#if defined( __AVR_ATmega1280__ )  // test disabled to save code size for 1280
		print_test_disabled();
		return (0);
	#else
		Serial.println_P(PSTR("Testing dataflash logging"));
		if (!DataFlash.CardInserted()) {
			Serial.println_P(PSTR("ERR: No dataflash inserted"));
			return 0;
		}
		DataFlash.ReadManufacturerID();
		Serial.printf_P(PSTR("Manufacturer: 0x%02x   Device: 0x%04x\n"),
						(unsigned)DataFlash.df_manufacturer,
						(unsigned)DataFlash.df_device);
		Serial.printf_P(PSTR("NumPages: %u  PageSize: %u\n"),
						(unsigned)DataFlash.df_NumPages+1,
						(unsigned)DataFlash.df_PageSize);
		DataFlash.StartRead(DataFlash.df_NumPages+1);
		Serial.printf_P(PSTR("Format version: %lx  Expected format version: %lx\n"),
						(unsigned long)DataFlash.ReadLong(), (unsigned long)DF_LOGGING_FORMAT);
		return 0;
	#endif
}


/*
static int8_t
//test_mission(uint8_t argc, const Menu::arg *argv)
{
	//write out a basic mission to the EEPROM

//{
//	uint8_t		id;					///< command id
//	uint8_t		options;			///< options bitmask (1<<0 = relative altitude)
//	uint8_t		p1;					///< param 1
//	int32_t		alt;				///< param 2 - Altitude in centimeters (meters * 100)
//	int32_t		lat;				///< param 3 - Lattitude * 10**7
//	int32_t		lng;				///< param 4 - Longitude * 10**7
//}

	// clear home
	{Location t = {0,   	0,	  0, 		0, 		0, 			0};
	set_cmd_with_index(t,0);}

	// CMD										opt						pitch   	alt/cm
	{Location t = {MAV_CMD_NAV_TAKEOFF,   		WP_OPTION_RELATIVE,	  0, 		100, 		0, 			0};
	set_cmd_with_index(t,1);}

	if (!strcmp_P(argv[1].str, PSTR("wp"))) {

		// CMD											opt
		{Location t = {MAV_CMD_NAV_WAYPOINT,  			WP_OPTION_RELATIVE,		15, 0, 0, 0};
		set_cmd_with_index(t,2);}
		// CMD											opt
		{Location t = {MAV_CMD_NAV_RETURN_TO_LAUNCH,   	WP_OPTION_YAW,	  0, 		0, 		0,		0};
		set_cmd_with_index(t,3);}

		// CMD											opt
		{Location t = {MAV_CMD_NAV_LAND,				0,	  0, 		0, 		0,		0};
		set_cmd_with_index(t,4);}

	} else {
		//2250 = 25 meteres
		// CMD										opt		p1		//alt		//NS		//WE
		{Location t = {MAV_CMD_NAV_LOITER_TIME,   	0,	  10,  	0, 			0,			0}; // 19
		set_cmd_with_index(t,2);}

		// CMD										opt		dir		angle/deg	deg/s	relative
		{Location t = {MAV_CMD_CONDITION_YAW,		0,	  1, 		360, 		60, 	1};
		set_cmd_with_index(t,3);}

		// CMD										opt
		{Location t = {MAV_CMD_NAV_LAND,			0,	  0, 		0, 			0, 		0};
		set_cmd_with_index(t,4);}

	}

	g.RTL_altitude.set_and_save(300);
	g.command_total.set_and_save(4);
	g.waypoint_radius.set_and_save(3);

	test_wp(NULL, NULL);
	return (0);
}
*/

static void print_hit_enter()
{
	Serial.printf_P(PSTR("Hit Enter to exit.\n\n"));
}

static void print_test_disabled()
{
	Serial.printf_P(PSTR("Sorry, not 1280 compat.\n"));
}

/*
//static void fake_out_gps()
{
	static float rads;
	g_gps->new_data 	= true;
	g_gps->fix	 	= true;

	//int length = g.rc_6.control_in;
	rads += .05;

	if (rads > 6.28){
		rads = 0;
	}

	g_gps->latitude	= 377696000;	// Y
	g_gps->longitude	= -1224319000;	// X
	g_gps->altitude	= 9000;			// meters * 100

	//next_WP.lng	 	= home.lng - length * sin(rads);   // X
	//next_WP.lat 	= home.lat + length * cos(rads);   // Y
}

*/
/*
//static void print_motor_out(){
	Serial.printf("out: R: %d,  L: %d  F: %d  B: %d\n",
				(motor_out[CH_1] 	- g.rc_3.radio_min),
				(motor_out[CH_2] 	- g.rc_3.radio_min),
				(motor_out[CH_3] 	- g.rc_3.radio_min),
				(motor_out[CH_4] 	- g.rc_3.radio_min));
}
*/
#endif // CLI_ENABLED