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https://github.com/ArduPilot/ardupilot
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uncrustify ArduPlane/radio.pde
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@ -75,7 +75,7 @@ static void read_radio()
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ch1_temp = APM_RC.InputCh(CH_ROLL);
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ch1_temp = APM_RC.InputCh(CH_ROLL);
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ch2_temp = APM_RC.InputCh(CH_PITCH);
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ch2_temp = APM_RC.InputCh(CH_PITCH);
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if(g.mix_mode == 0){
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if(g.mix_mode == 0) {
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g.channel_roll.set_pwm(ch1_temp);
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g.channel_roll.set_pwm(ch1_temp);
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g.channel_pitch.set_pwm(ch2_temp);
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g.channel_pitch.set_pwm(ch2_temp);
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}else{
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}else{
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@ -106,11 +106,11 @@ static void read_radio()
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}
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}
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/*
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/*
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Serial.printf_P(PSTR("OUT 1: %d\t2: %d\t3: %d\t4: %d \n"),
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* Serial.printf_P(PSTR("OUT 1: %d\t2: %d\t3: %d\t4: %d \n"),
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(int)g.rc_1.control_in,
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* (int)g.rc_1.control_in,
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(int)g.rc_2.control_in,
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* (int)g.rc_2.control_in,
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(int)g.rc_3.control_in,
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* (int)g.rc_3.control_in,
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(int)g.rc_4.control_in);
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* (int)g.rc_4.control_in);
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*/
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*/
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}
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}
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@ -129,30 +129,30 @@ static void control_failsafe(uint16_t pwm)
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//Check for failsafe and debounce funky reads
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//Check for failsafe and debounce funky reads
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} else if (g.throttle_fs_enabled) {
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} else if (g.throttle_fs_enabled) {
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if (pwm < (unsigned)g.throttle_fs_value){
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if (pwm < (unsigned)g.throttle_fs_value) {
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// we detect a failsafe from radio
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// we detect a failsafe from radio
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// throttle has dropped below the mark
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// throttle has dropped below the mark
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failsafeCounter++;
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failsafeCounter++;
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if (failsafeCounter == 9){
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if (failsafeCounter == 9) {
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gcs_send_text_fmt(PSTR("MSG FS ON %u"), (unsigned)pwm);
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gcs_send_text_fmt(PSTR("MSG FS ON %u"), (unsigned)pwm);
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}else if(failsafeCounter == 10) {
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}else if(failsafeCounter == 10) {
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ch3_failsafe = true;
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ch3_failsafe = true;
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}else if (failsafeCounter > 10){
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}else if (failsafeCounter > 10) {
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failsafeCounter = 11;
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failsafeCounter = 11;
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}
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}
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}else if(failsafeCounter > 0){
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}else if(failsafeCounter > 0) {
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// we are no longer in failsafe condition
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// we are no longer in failsafe condition
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// but we need to recover quickly
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// but we need to recover quickly
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failsafeCounter--;
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failsafeCounter--;
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if (failsafeCounter > 3){
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if (failsafeCounter > 3) {
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failsafeCounter = 3;
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failsafeCounter = 3;
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}
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}
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if (failsafeCounter == 1){
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if (failsafeCounter == 1) {
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gcs_send_text_fmt(PSTR("MSG FS OFF %u"), (unsigned)pwm);
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gcs_send_text_fmt(PSTR("MSG FS OFF %u"), (unsigned)pwm);
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}else if(failsafeCounter == 0) {
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}else if(failsafeCounter == 0) {
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ch3_failsafe = false;
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ch3_failsafe = false;
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}else if (failsafeCounter <0){
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}else if (failsafeCounter <0) {
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failsafeCounter = -1;
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failsafeCounter = -1;
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}
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}
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}
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}
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@ -164,7 +164,7 @@ static void trim_control_surfaces()
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read_radio();
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read_radio();
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// Store control surface trim values
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// Store control surface trim values
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// ---------------------------------
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// ---------------------------------
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if(g.mix_mode == 0){
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if(g.mix_mode == 0) {
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g.channel_roll.radio_trim = g.channel_roll.radio_in;
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g.channel_roll.radio_trim = g.channel_roll.radio_in;
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g.channel_pitch.radio_trim = g.channel_pitch.radio_in;
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g.channel_pitch.radio_trim = g.channel_pitch.radio_in;
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G_RC_AUX(k_aileron)->radio_trim = g_rc_function[RC_Channel_aux::k_aileron]->radio_in; // Second aileron channel
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G_RC_AUX(k_aileron)->radio_trim = g_rc_function[RC_Channel_aux::k_aileron]->radio_in; // Second aileron channel
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@ -196,7 +196,7 @@ static void trim_radio()
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// Store the trim values
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// Store the trim values
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// ---------------------
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// ---------------------
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if(g.mix_mode == 0){
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if(g.mix_mode == 0) {
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g.channel_roll.radio_trim = g.channel_roll.radio_in;
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g.channel_roll.radio_trim = g.channel_roll.radio_in;
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g.channel_pitch.radio_trim = g.channel_pitch.radio_in;
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g.channel_pitch.radio_trim = g.channel_pitch.radio_in;
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//g.channel_throttle.radio_trim = g.channel_throttle.radio_in;
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//g.channel_throttle.radio_trim = g.channel_throttle.radio_in;
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