ardupilot/ArduPlane/radio.pde

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// -*- tab-width: 4; Mode: C++; c-basic-offset: 4; indent-tabs-mode: nil -*-
//Function that will read the radio data, limit servos and trigger a failsafe
// ----------------------------------------------------------------------------
static uint8_t failsafeCounter = 0; // we wait a second to take over the throttle and send the plane circling
extern RC_Channel* rc_ch[8];
static void init_rc_in()
{
// set rc channel ranges
g.channel_roll.set_angle(SERVO_MAX);
g.channel_pitch.set_angle(SERVO_MAX);
g.channel_rudder.set_angle(SERVO_MAX);
g.channel_throttle.set_range(0, 100);
// set rc dead zones
g.channel_roll.set_dead_zone(60);
g.channel_pitch.set_dead_zone(60);
g.channel_rudder.set_dead_zone(60);
g.channel_throttle.set_dead_zone(6);
//g.channel_roll.dead_zone = 60;
//g.channel_pitch.dead_zone = 60;
//g.channel_rudder.dead_zone = 60;
//g.channel_throttle.dead_zone = 6;
rc_ch[CH_1] = &g.channel_roll;
rc_ch[CH_2] = &g.channel_pitch;
rc_ch[CH_3] = &g.channel_throttle;
rc_ch[CH_4] = &g.channel_rudder;
rc_ch[CH_5] = &g.rc_5;
rc_ch[CH_6] = &g.rc_6;
rc_ch[CH_7] = &g.rc_7;
rc_ch[CH_8] = &g.rc_8;
//set auxiliary ranges
#if CONFIG_HAL_BOARD == HAL_BOARD_APM2
update_aux_servo_function(&g.rc_5, &g.rc_6, &g.rc_7, &g.rc_8, &g.rc_9, &g.rc_10, &g.rc_11);
#else
update_aux_servo_function(&g.rc_5, &g.rc_6, &g.rc_7, &g.rc_8);
#endif
}
static void init_rc_out()
{
hal.rcout->enable_ch(CH_1);
hal.rcout->enable_ch(CH_2);
hal.rcout->enable_ch(CH_3);
hal.rcout->enable_ch(CH_4);
enable_aux_servos();
// Initialization of servo outputs
hal.rcout->write(CH_1, g.channel_roll.radio_trim);
hal.rcout->write(CH_2, g.channel_pitch.radio_trim);
hal.rcout->write(CH_3, g.channel_throttle.radio_min);
hal.rcout->write(CH_4, g.channel_rudder.radio_trim);
hal.rcout->write(CH_5, g.rc_5.radio_trim);
hal.rcout->write(CH_6, g.rc_6.radio_trim);
hal.rcout->write(CH_7, g.rc_7.radio_trim);
hal.rcout->write(CH_8, g.rc_8.radio_trim);
#if CONFIG_HAL_BOARD == HAL_BOARD_APM2
hal.rcout->write(CH_9, g.rc_9.radio_trim);
hal.rcout->write(CH_10, g.rc_10.radio_trim);
hal.rcout->write(CH_11, g.rc_11.radio_trim);
#endif
}
static void read_radio()
{
ch1_temp = hal.rcin->read(CH_ROLL);
ch2_temp = hal.rcin->read(CH_PITCH);
if(g.mix_mode == 0) {
g.channel_roll.set_pwm(ch1_temp);
g.channel_pitch.set_pwm(ch2_temp);
}else{
g.channel_roll.set_pwm(BOOL_TO_SIGN(g.reverse_elevons) * (BOOL_TO_SIGN(g.reverse_ch2_elevon) * int(ch2_temp - elevon2_trim) - BOOL_TO_SIGN(g.reverse_ch1_elevon) * int(ch1_temp - elevon1_trim)) / 2 + 1500);
g.channel_pitch.set_pwm((BOOL_TO_SIGN(g.reverse_ch2_elevon) * int(ch2_temp - elevon2_trim) + BOOL_TO_SIGN(g.reverse_ch1_elevon) * int(ch1_temp - elevon1_trim)) / 2 + 1500);
}
g.channel_throttle.set_pwm(hal.rcin->read(CH_3));
g.channel_rudder.set_pwm(hal.rcin->read(CH_4));
g.rc_5.set_pwm(hal.rcin->read(CH_5));
g.rc_6.set_pwm(hal.rcin->read(CH_6));
g.rc_7.set_pwm(hal.rcin->read(CH_7));
g.rc_8.set_pwm(hal.rcin->read(CH_8));
control_failsafe(g.channel_throttle.radio_in);
g.channel_throttle.servo_out = g.channel_throttle.control_in;
if (g.throttle_nudge && g.channel_throttle.servo_out > 50) {
float nudge = (g.channel_throttle.servo_out - 50) * 0.02;
if (alt_control_airspeed()) {
airspeed_nudge_cm = (g.flybywire_airspeed_max * 100 - g.airspeed_cruise_cm) * nudge;
} else {
throttle_nudge = (g.throttle_max - g.throttle_cruise) * nudge;
}
} else {
airspeed_nudge_cm = 0;
throttle_nudge = 0;
}
/*
* cliSerial->printf_P(PSTR("OUT 1: %d\t2: %d\t3: %d\t4: %d \n"),
* (int)g.rc_1.control_in,
* (int)g.rc_2.control_in,
* (int)g.rc_3.control_in,
* (int)g.rc_4.control_in);
*/
}
static void control_failsafe(uint16_t pwm)
{
if(g.throttle_fs_enabled == 0)
return;
// Check for failsafe condition based on loss of GCS control
if (rc_override_active) {
if(millis() - rc_override_fs_timer > FAILSAFE_SHORT_TIME) {
ch3_failsafe = true;
} else {
ch3_failsafe = false;
}
//Check for failsafe and debounce funky reads
} else if (g.throttle_fs_enabled) {
if (pwm < (unsigned)g.throttle_fs_value) {
// we detect a failsafe from radio
// throttle has dropped below the mark
failsafeCounter++;
if (failsafeCounter == 9) {
gcs_send_text_fmt(PSTR("MSG FS ON %u"), (unsigned)pwm);
}else if(failsafeCounter == 10) {
ch3_failsafe = true;
}else if (failsafeCounter > 10) {
failsafeCounter = 11;
}
}else if(failsafeCounter > 0) {
// we are no longer in failsafe condition
// but we need to recover quickly
failsafeCounter--;
if (failsafeCounter > 3) {
failsafeCounter = 3;
}
if (failsafeCounter == 1) {
gcs_send_text_fmt(PSTR("MSG FS OFF %u"), (unsigned)pwm);
}else if(failsafeCounter == 0) {
ch3_failsafe = false;
}else if (failsafeCounter <0) {
failsafeCounter = -1;
}
}
}
}
static void trim_control_surfaces()
{
read_radio();
// Store control surface trim values
// ---------------------------------
if(g.mix_mode == 0) {
g.channel_roll.radio_trim = g.channel_roll.radio_in;
g.channel_pitch.radio_trim = g.channel_pitch.radio_in;
// the secondary aileron is trimmed only if it has a
// corresponding transmitter input channel, which k_aileron
// doesn't have
RC_Channel_aux::set_radio_trim(RC_Channel_aux::k_aileron_with_input);
} else{
elevon1_trim = ch1_temp;
elevon2_trim = ch2_temp;
//Recompute values here using new values for elevon1_trim and elevon2_trim
//We cannot use radio_in[CH_ROLL] and radio_in[CH_PITCH] values from read_radio() because the elevon trim values have changed
uint16_t center = 1500;
g.channel_roll.radio_trim = center;
g.channel_pitch.radio_trim = center;
}
g.channel_rudder.radio_trim = g.channel_rudder.radio_in;
// save to eeprom
g.channel_roll.save_eeprom();
g.channel_pitch.save_eeprom();
g.channel_rudder.save_eeprom();
}
static void trim_radio()
{
for (uint8_t y = 0; y < 30; y++) {
read_radio();
}
trim_control_surfaces();
}