mirror of https://github.com/ArduPilot/ardupilot
221 lines
6.5 KiB
Plaintext
221 lines
6.5 KiB
Plaintext
// -*- tab-width: 4; Mode: C++; c-basic-offset: 4; indent-tabs-mode: nil -*-
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// Function that will read the radio data, limit servos and trigger a failsafe
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// ----------------------------------------------------------------------------
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extern RC_Channel* rc_ch[8];
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static void default_dead_zones()
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{
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g.rc_1.set_dead_zone(60);
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g.rc_2.set_dead_zone(60);
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#if FRAME_CONFIG == HELI_FRAME
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g.rc_3.set_dead_zone(20);
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g.rc_4.set_dead_zone(30);
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#else
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g.rc_3.set_dead_zone(60);
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g.rc_4.set_dead_zone(80);
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#endif
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g.rc_6.set_dead_zone(0);
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}
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static void init_rc_in()
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{
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// set rc channel ranges
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g.rc_1.set_angle(MAX_INPUT_ROLL_ANGLE);
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g.rc_2.set_angle(MAX_INPUT_PITCH_ANGLE);
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#if FRAME_CONFIG == HELI_FRAME
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// we do not want to limit the movment of the heli's swash plate
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g.rc_3.set_range(0, 1000);
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#else
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g.rc_3.set_range(g.throttle_min, g.throttle_max);
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#endif
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g.rc_4.set_angle(4500);
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// reverse: CW = left
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// normal: CW = left???
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g.rc_1.set_type(RC_CHANNEL_TYPE_ANGLE_RAW);
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g.rc_2.set_type(RC_CHANNEL_TYPE_ANGLE_RAW);
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g.rc_4.set_type(RC_CHANNEL_TYPE_ANGLE_RAW);
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rc_ch[CH_1] = &g.rc_1;
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rc_ch[CH_2] = &g.rc_2;
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rc_ch[CH_3] = &g.rc_3;
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rc_ch[CH_4] = &g.rc_4;
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rc_ch[CH_5] = &g.rc_5;
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rc_ch[CH_6] = &g.rc_6;
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rc_ch[CH_7] = &g.rc_7;
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rc_ch[CH_8] = &g.rc_8;
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//set auxiliary ranges
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g.rc_5.set_range(0,1000);
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g.rc_6.set_range(0,1000);
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g.rc_7.set_range(0,1000);
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g.rc_8.set_range(0,1000);
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#if CONFIG_HAL_BOARD == HAL_BOARD_PX4
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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, &g.rc_12);
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#elif MOUNT == ENABLED
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update_aux_servo_function(&g.rc_5, &g.rc_6, &g.rc_7, &g.rc_8, &g.rc_10, &g.rc_11);
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#endif
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}
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// init_rc_out -- initialise motors and check if pilot wants to perform ESC calibration
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static void init_rc_out()
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{
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motors.set_update_rate(g.rc_speed);
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motors.set_frame_orientation(g.frame_orientation);
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motors.Init(); // motor initialisation
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motors.set_min_throttle(g.throttle_min);
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motors.set_max_throttle(g.throttle_max);
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for(uint8_t i = 0; i < 5; i++) {
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delay(20);
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read_radio();
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}
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// we want the input to be scaled correctly
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g.rc_3.set_range_out(0,1000);
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// full throttle means to enter ESC calibration
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if(g.rc_3.control_in >= (MAXIMUM_THROTTLE - 50)) {
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if(g.esc_calibrate == 0) {
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// we will enter esc_calibrate mode on next reboot
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g.esc_calibrate.set_and_save(1);
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// display message on console
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cliSerial->printf_P(PSTR("Entering ESC Calibration: please restart APM.\n"));
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// block until we restart
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while(1) {
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delay(200);
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dancing_light();
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}
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}else{
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cliSerial->printf_P(PSTR("ESC Calibration active: passing throttle through to ESCs.\n"));
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// clear esc flag
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g.esc_calibrate.set_and_save(0);
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// pass through user throttle to escs
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init_esc();
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}
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}else{
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// did we abort the calibration?
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if(g.esc_calibrate == 1)
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g.esc_calibrate.set_and_save(0);
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}
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// enable output to motors
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pre_arm_rc_checks();
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if (ap.pre_arm_rc_check) {
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output_min();
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}
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#if TOY_EDF == ENABLED
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// add access to CH8 and CH6
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APM_RC.enable_out(CH_8);
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APM_RC.enable_out(CH_6);
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#endif
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}
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// output_min - enable and output lowest possible value to motors
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void output_min()
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{
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// enable motors
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motors.enable();
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motors.output_min();
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}
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#define FAILSAFE_RADIO_TIMEOUT_MS 2000 // 2 seconds
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static void read_radio()
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{
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static uint32_t last_update = 0;
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if (hal.rcin->valid_channels() > 0) {
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last_update = millis();
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ap_system.new_radio_frame = true;
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uint16_t periods[8];
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hal.rcin->read(periods,8);
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g.rc_1.set_pwm(periods[0]);
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g.rc_2.set_pwm(periods[1]);
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set_throttle_and_failsafe(periods[2]);
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g.rc_4.set_pwm(periods[3]);
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g.rc_5.set_pwm(periods[4]);
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g.rc_6.set_pwm(periods[5]);
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g.rc_7.set_pwm(periods[6]);
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g.rc_8.set_pwm(periods[7]);
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#if FRAME_CONFIG != HELI_FRAME
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// limit our input to 800 so we can still pitch and roll
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g.rc_3.control_in = min(g.rc_3.control_in, MAXIMUM_THROTTLE);
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#endif
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}else{
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uint32_t elapsed = millis() - last_update;
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// turn on throttle failsafe if no update from ppm encoder for 2 seconds
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if ((elapsed >= FAILSAFE_RADIO_TIMEOUT_MS)
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&& g.failsafe_throttle && motors.armed() && !ap.failsafe_radio) {
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Log_Write_Error(ERROR_SUBSYSTEM_RADIO, ERROR_CODE_RADIO_LATE_FRAME);
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set_failsafe_radio(true);
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}
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}
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}
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#define FS_COUNTER 3
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static void set_throttle_and_failsafe(uint16_t throttle_pwm)
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{
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static int8_t failsafe_counter = 0;
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// if failsafe not enabled pass through throttle and exit
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if(g.failsafe_throttle == FS_THR_DISABLED) {
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g.rc_3.set_pwm(throttle_pwm);
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return;
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}
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//check for low throttle value
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if (throttle_pwm < (uint16_t)g.failsafe_throttle_value) {
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// if we are already in failsafe or motors not armed pass through throttle and exit
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if (ap.failsafe_radio || !motors.armed()) {
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g.rc_3.set_pwm(throttle_pwm);
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return;
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}
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// check for 3 low throttle values
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// Note: we do not pass through the low throttle until 3 low throttle values are recieved
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failsafe_counter++;
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if( failsafe_counter >= FS_COUNTER ) {
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failsafe_counter = FS_COUNTER; // check to ensure we don't overflow the counter
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set_failsafe_radio(true);
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g.rc_3.set_pwm(throttle_pwm); // pass through failsafe throttle
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}
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}else{
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// we have a good throttle so reduce failsafe counter
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failsafe_counter--;
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if( failsafe_counter <= 0 ) {
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failsafe_counter = 0; // check to ensure we don't underflow the counter
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// disengage failsafe after three (nearly) consecutive valid throttle values
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if (ap.failsafe_radio) {
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set_failsafe_radio(false);
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}
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}
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// pass through throttle
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g.rc_3.set_pwm(throttle_pwm);
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}
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}
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static void trim_radio()
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{
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for (uint8_t i = 0; i < 30; i++) {
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read_radio();
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}
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g.rc_1.trim(); // roll
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g.rc_2.trim(); // pitch
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g.rc_4.trim(); // yaw
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g.rc_1.save_eeprom();
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g.rc_2.save_eeprom();
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g.rc_4.save_eeprom();
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}
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