ardupilot/ArduCopterMega/radio.pde

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void init_radio()
{
rc_1.set_angle(4500);
rc_1.dead_zone = 50;
rc_2.set_angle(4500);
rc_2.dead_zone = 50;
rc_3.set_range(0,1000);
rc_3.dead_zone = 20;
rc_3.radio_max += 300; // hack for better throttle control
rc_4.set_angle(6000);
rc_4.dead_zone = 500;
rc_5.set_range(0,1000);
rc_5.set_filter(false);
rc_6.set_range(50,200);
rc_7.set_range(0,1000);
rc_8.set_range(0,1000);
#if ARM_AT_STARTUP == 1
motor_armed = 1;
#endif
APM_RC.OutputCh(CH_1, rc_3.radio_min); // Initialization of servo outputs
APM_RC.OutputCh(CH_2, rc_3.radio_min);
APM_RC.OutputCh(CH_3, rc_3.radio_min);
APM_RC.OutputCh(CH_4, rc_3.radio_min);
APM_RC.Init(); // APM Radio initialization
APM_RC.OutputCh(CH_1, rc_3.radio_min); // Initialization of servo outputs
APM_RC.OutputCh(CH_2, rc_3.radio_min);
APM_RC.OutputCh(CH_3, rc_3.radio_min);
APM_RC.OutputCh(CH_4, rc_3.radio_min);
}
void read_radio()
{
rc_1.set_pwm(APM_RC.InputCh(CH_1));
rc_2.set_pwm(APM_RC.InputCh(CH_2));
rc_3.set_pwm(APM_RC.InputCh(CH_3));
rc_4.set_pwm(APM_RC.InputCh(CH_4));
rc_5.set_pwm(APM_RC.InputCh(CH_5));
rc_6.set_pwm(APM_RC.InputCh(CH_6));
rc_7.set_pwm(APM_RC.InputCh(CH_7));
rc_8.set_pwm(APM_RC.InputCh(CH_8));
//Serial.printf_P(PSTR("OUT 1: %d\t2: %d\t3: %d\t4: %d \n"), rc_1.control_in, rc_2.control_in, rc_3.control_in, rc_4.control_in);
}
void trim_radio()
{
read_radio();
rc_1.trim(); // roll
rc_2.trim(); // pitch
rc_4.trim(); // yaw
}
#define ARM_DELAY 10
#define DISARM_DELAY 10
void arm_motors()
{
static byte arming_counter;
// Arm motor output : Throttle down and full yaw right for more than 2 seconds
if (rc_3.control_in == 0){
if (rc_4.control_in > 2700) {
if (arming_counter > ARM_DELAY) {
motor_armed = true;
} else{
arming_counter++;
}
}else if (rc_4.control_in < -2700) {
if (arming_counter > DISARM_DELAY){
motor_armed = false;
}else{
arming_counter++;
}
}else{
arming_counter = 0;
}
}
}