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

#if FRAME_CONFIG ==	HELI_FRAME

static int heli_manual_override = false;
static float rollPitch_impact_on_collective = 0;

static void heli_init_swash()
{
    int i;
	int tilt_max[CH_3+1];
	int total_tilt_max = 0;
	
	// swash servo initialisation
	g.heli_servo_1.set_range(0,1000);
	g.heli_servo_2.set_range(0,1000);
	g.heli_servo_3.set_range(0,1000);
	g.heli_servo_4.set_angle(4500);
	//g.heli_servo_4.radio_min = 1000;  // required?
	//g.heli_servo_4.radio_max = 2000;
	
	// pitch factors
	heli_pitchFactor[CH_1] = cos(radians(g.heli_servo1_pos));
	heli_pitchFactor[CH_2] = cos(radians(g.heli_servo2_pos));
	heli_pitchFactor[CH_3] = cos(radians(g.heli_servo3_pos));
	
	// roll factors
    heli_rollFactor[CH_1] = cos(radians(g.heli_servo1_pos + 90));
	heli_rollFactor[CH_2] = cos(radians(g.heli_servo2_pos + 90));
	heli_rollFactor[CH_3] = cos(radians(g.heli_servo3_pos + 90));
	
	// collective min / max
	total_tilt_max = 0;
	for( i=CH_1; i<=CH_3; i++ ) {
	    tilt_max[i] = max(abs(heli_rollFactor[i]*g.heli_roll_max), abs(heli_pitchFactor[i]*g.heli_pitch_max))/100;
		total_tilt_max = max(total_tilt_max,tilt_max[i]);
	}
	
	//if( reset_collective == false ) {
	//	g.heli_coll_min = total_tilt_max;
	//	g.heli_coll_max = 1000 - total_tilt_max;
	//}
	
	// servo min/max values - or should I use set_range?
	g.heli_servo_1.radio_min = g.heli_coll_min - tilt_max[CH_1];
	g.heli_servo_1.radio_max = g.heli_coll_max + tilt_max[CH_1];
	g.heli_servo_2.radio_min = g.heli_coll_min - tilt_max[CH_2];
	g.heli_servo_2.radio_max = g.heli_coll_max + tilt_max[CH_2];
	g.heli_servo_3.radio_min = g.heli_coll_min - tilt_max[CH_3];
	g.heli_servo_3.radio_max = g.heli_coll_max + tilt_max[CH_3];
}

static void heli_move_servos_to_mid()
{
	heli_move_swash(0,0,1500,0);
}

//
// heli_move_swash - moves swash plate to attitude of parameters passed in
//                 - expected ranges:
//                       roll : -4500 ~ 4500   // should be -500 to 500?
//                       pitch: -4500 ~ 4500
//                       collective: 1000 ~ 2000
//                       yaw:   -4500 ~ 4500??
//
static void heli_move_swash(int roll_out, int pitch_out, int coll_out, int yaw_out)
{
    // ensure values are acceptable:
	roll_out = constrain(roll_out, (int)-g.heli_roll_max, (int)g.heli_roll_max);
	pitch_out = constrain(pitch_out, (int)-g.heli_pitch_max, (int)g.heli_pitch_max);
	coll_out = constrain(coll_out, (int)g.heli_coll_min, (int)g.heli_coll_max);

	// swashplate servos
	g.heli_servo_1.servo_out = (heli_rollFactor[CH_1] * roll_out + heli_pitchFactor[CH_1] * pitch_out)/10 + coll_out + (g.heli_servo_1.radio_trim-1500);
	if( g.heli_servo_1.get_reverse() )
	    g.heli_servo_1.servo_out = 3000 - g.heli_servo_1.servo_out;
		
	g.heli_servo_2.servo_out = (heli_rollFactor[CH_2] * roll_out + heli_pitchFactor[CH_2] * pitch_out)/10 + coll_out + (g.heli_servo_2.radio_trim-1500);
	if( g.heli_servo_2.get_reverse() )
		g.heli_servo_2.servo_out = 3000 - g.heli_servo_2.servo_out;
		
	g.heli_servo_3.servo_out = (heli_rollFactor[CH_3] * roll_out + heli_pitchFactor[CH_3] * pitch_out)/10 + coll_out + (g.heli_servo_3.radio_trim-1500);
	if( g.heli_servo_3.get_reverse() )
	    g.heli_servo_3.servo_out = 3000 - g.heli_servo_3.servo_out;
		
	if( g.heli_servo_4.get_reverse() )
		g.heli_servo_4.servo_out = -yaw_out;  // should probably just use rc_4 directly like we do for a tricopter
	else
		g.heli_servo_4.servo_out = yaw_out;
	
	// use servo_out to calculate pwm_out and radio_out
	g.heli_servo_1.calc_pwm();
	g.heli_servo_2.calc_pwm();
	g.heli_servo_3.calc_pwm();
	g.heli_servo_4.calc_pwm();	
	
	// actually move the servos
	APM_RC.OutputCh(CH_1, g.heli_servo_1.servo_out);
	APM_RC.OutputCh(CH_2, g.heli_servo_2.servo_out);
	APM_RC.OutputCh(CH_3, g.heli_servo_3.servo_out);
	//APM_RC.OutputCh(CH_4, g.heli_servo_4.servo_out);
	APM_RC.OutputCh(CH_4, g.heli_servo_4.radio_out);
	
	// output gyro value
	if( g.heli_ext_gyro_enabled ) {
	    APM_RC.OutputCh(CH_7, g.heli_ext_gyro_gain);
	}

	// InstantPWM
	APM_RC.Force_Out0_Out1();
	APM_RC.Force_Out2_Out3();
	
	// debug
	//Serial.printf_P(PSTR("4: r%d \tcp:%d \tcol:%d \ty:%d \tout:%d \tpwm:%d \trOut:%d \ttrim:%d\n"), roll_out, pitch_out, coll_out, yaw_out, (int)g.heli_servo_4.servo_out, (int)g.heli_servo_4.pwm_out, (int)g.heli_servo_4.radio_out, (int)g.heli_servo_4.radio_trim);
	//Serial.printf_P(PSTR("4: y:%d \tout:%d \tpwm:%d \trOut:%d \ttrim:%d\n"), yaw_out, (int)g.heli_servo_4.servo_out, (int)g.heli_servo_4.pwm_out, (int)g.heli_servo_4.radio_out, (int)g.heli_servo_4.radio_trim);
	//Serial.printf_P(PSTR("4: y:%d \tro:%d\n"), yaw_out, (int)g.heli_servo_4.radio_out);
}

// these are not really motors, they're servos but we don't rename the function because it fits with the rest of the code better
static void output_motors_armed()
{
    //static int counter = 0;
	g.rc_1.calc_pwm();
	g.rc_2.calc_pwm();
	g.rc_3.calc_pwm();
	g.rc_4.calc_pwm();

	if( heli_manual_override ) {
	    // straight pass through from radio inputs to swash plate
	    heli_move_swash( g.rc_1.control_in, g.rc_2.control_in, g.rc_3.radio_in, g.rc_4.control_in );
		
	    /*Serial.printf_P(  PSTR("1: %d/%d \t2:%d/%d \t3:%d/%d \t4:%d/%d\n"), 
			(int)g.rc_1.control_in, (int)g.rc_1.servo_out, 
			(int)g.rc_2.control_in, (int)g.rc_2.servo_out, 
			(int)g.rc_3.radio_in,   (int)g.rc_3.servo_out, 
			(int)g.rc_4.control_in, (int)g.rc_4.servo_out );*/
	}else{
	    // collective pitch compensation for yaw/roll.  This probably belongs somewhere else
		//Matrix3f temp 	= dcm.get_dcm_matrix();
		//rollPitch_impact_on_collective = 1.0 * (g.rc_3.radio_in-g.heli_coll_mid) * (1.0 - temp.c.z);
		//rollPitch_impact_on_collective = constrain(rollPitch_impact_on_collective,0,100);
		
		/*counter++;
		if( counter > 20 ) {
		    counter = 0;
			Serial.printf_P( PSTR("dcm:%f4.1\t rc3:%d\t cm:%d\t imp:%d\n"), 
				temp.c.z, 
				(int)g.rc_3.radio_in,
				(int)g.heli_coll_mid,
				(int)rollPitch_impact_on_collective );
		}*/
	
	    // source inputs from attitude controller (except for collective pitch)
	    //heli_move_swash( g.rc_1.servo_out, g.rc_2.servo_out, g.rc_3.radio_in + rollPitch_impact_on_collective, g.rc_4.servo_out );  // to allow control by PIDs except for collective
		heli_move_swash( g.rc_1.servo_out, g.rc_2.servo_out, g.rc_3.radio_out, g.rc_4.servo_out );  // to allow control by PIDs except for collective
	}
}

// for helis - armed or disarmed we allow servos to move
static void output_motors_disarmed()
{
	if(g.rc_3.control_in > 0){
		// we have pushed up the throttle
		// remove safety
		motor_auto_armed = true;
	}

	output_motors_armed();
}

static void output_motor_test()
{
}

#endif // HELI_FRAME