mirror of https://github.com/ArduPilot/ardupilot
189 lines
6.2 KiB
Plaintext
189 lines
6.2 KiB
Plaintext
// -*- 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 void default_dead_zones()
|
|
{
|
|
g.rc_1.set_default_dead_zone(30);
|
|
g.rc_2.set_default_dead_zone(30);
|
|
#if FRAME_CONFIG == HELI_FRAME
|
|
g.rc_3.set_default_dead_zone(10);
|
|
g.rc_4.set_default_dead_zone(15);
|
|
g.rc_8.set_default_dead_zone(10);
|
|
#else
|
|
g.rc_3.set_default_dead_zone(30);
|
|
g.rc_4.set_default_dead_zone(40);
|
|
#endif
|
|
g.rc_6.set_default_dead_zone(0);
|
|
}
|
|
|
|
static void init_rc_in()
|
|
{
|
|
// set rc channel ranges
|
|
g.rc_1.set_angle(ROLL_PITCH_INPUT_MAX);
|
|
g.rc_2.set_angle(ROLL_PITCH_INPUT_MAX);
|
|
g.rc_3.set_range(g.throttle_min, THR_MAX);
|
|
g.rc_4.set_angle(4500);
|
|
|
|
g.rc_1.set_type(RC_CHANNEL_TYPE_ANGLE_RAW);
|
|
g.rc_2.set_type(RC_CHANNEL_TYPE_ANGLE_RAW);
|
|
g.rc_4.set_type(RC_CHANNEL_TYPE_ANGLE_RAW);
|
|
|
|
//set auxiliary servo ranges
|
|
g.rc_5.set_range(0,1000);
|
|
g.rc_6.set_range(0,1000);
|
|
g.rc_7.set_range(0,1000);
|
|
g.rc_8.set_range(0,1000);
|
|
|
|
// set default dead zones
|
|
default_dead_zones();
|
|
|
|
// initialise throttle_zero flag
|
|
ap.throttle_zero = true;
|
|
}
|
|
|
|
// init_rc_out -- initialise motors and check if pilot wants to perform ESC calibration
|
|
static void init_rc_out()
|
|
{
|
|
motors.set_update_rate(g.rc_speed);
|
|
motors.set_frame_orientation(g.frame_orientation);
|
|
motors.Init(); // motor initialisation
|
|
motors.set_min_throttle(g.throttle_min);
|
|
|
|
for(uint8_t i = 0; i < 5; i++) {
|
|
delay(20);
|
|
read_radio();
|
|
}
|
|
|
|
// we want the input to be scaled correctly
|
|
g.rc_3.set_range_out(0,1000);
|
|
|
|
// check if we should enter esc calibration mode
|
|
esc_calibration_startup_check();
|
|
|
|
// enable output to motors
|
|
pre_arm_rc_checks();
|
|
if (ap.pre_arm_rc_check) {
|
|
output_min();
|
|
}
|
|
|
|
// setup correct scaling for ESCs like the UAVCAN PX4ESC which
|
|
// take a proportion of speed. Note: this assumes rc_3 is
|
|
// throttle and should really use rcmap.
|
|
hal.rcout->set_esc_scaling(g.rc_3.radio_min, g.rc_3.radio_max);
|
|
}
|
|
|
|
// output_min - enable and output lowest possible value to motors
|
|
void output_min()
|
|
{
|
|
// enable motors
|
|
motors.enable();
|
|
motors.output_min();
|
|
}
|
|
|
|
static void read_radio()
|
|
{
|
|
static uint32_t last_update_ms = 0;
|
|
uint32_t tnow_ms = millis();
|
|
|
|
if (hal.rcin->new_input()) {
|
|
last_update_ms = tnow_ms;
|
|
ap.new_radio_frame = true;
|
|
uint16_t periods[8];
|
|
hal.rcin->read(periods,8);
|
|
g.rc_1.set_pwm(periods[rcmap.roll()-1]);
|
|
g.rc_2.set_pwm(periods[rcmap.pitch()-1]);
|
|
|
|
set_throttle_and_failsafe(periods[rcmap.throttle()-1]);
|
|
set_throttle_zero_flag(g.rc_3.control_in);
|
|
|
|
g.rc_4.set_pwm(periods[rcmap.yaw()-1]);
|
|
g.rc_5.set_pwm(periods[4]);
|
|
g.rc_6.set_pwm(periods[5]);
|
|
g.rc_7.set_pwm(periods[6]);
|
|
g.rc_8.set_pwm(periods[7]);
|
|
|
|
// read channels 9 ~ 14
|
|
for (uint8_t i=8; i<RC_MAX_CHANNELS; i++) {
|
|
if (RC_Channel::rc_channel(i) != NULL) {
|
|
RC_Channel::rc_channel(i)->set_pwm(RC_Channel::rc_channel(i)->read());
|
|
}
|
|
}
|
|
|
|
// flag we must have an rc receiver attached
|
|
if (!failsafe.rc_override_active) {
|
|
ap.rc_receiver_present = true;
|
|
}
|
|
|
|
// update output on any aux channels, for manual passthru
|
|
RC_Channel_aux::output_ch_all();
|
|
}else{
|
|
uint32_t elapsed = tnow_ms - last_update_ms;
|
|
// turn on throttle failsafe if no update from the RC Radio for 500ms or 2000ms if we are using RC_OVERRIDE
|
|
if (((!failsafe.rc_override_active && (elapsed >= FS_RADIO_TIMEOUT_MS)) || (failsafe.rc_override_active && (elapsed >= FS_RADIO_RC_OVERRIDE_TIMEOUT_MS))) &&
|
|
(g.failsafe_throttle && (ap.rc_receiver_present||motors.armed()) && !failsafe.radio)) {
|
|
Log_Write_Error(ERROR_SUBSYSTEM_RADIO, ERROR_CODE_RADIO_LATE_FRAME);
|
|
set_failsafe_radio(true);
|
|
}
|
|
}
|
|
}
|
|
|
|
#define FS_COUNTER 3 // radio failsafe kicks in after 3 consecutive throttle values below failsafe_throttle_value
|
|
static void set_throttle_and_failsafe(uint16_t throttle_pwm)
|
|
{
|
|
// if failsafe not enabled pass through throttle and exit
|
|
if(g.failsafe_throttle == FS_THR_DISABLED) {
|
|
g.rc_3.set_pwm(throttle_pwm);
|
|
return;
|
|
}
|
|
|
|
//check for low throttle value
|
|
if (throttle_pwm < (uint16_t)g.failsafe_throttle_value) {
|
|
|
|
// if we are already in failsafe or motors not armed pass through throttle and exit
|
|
if (failsafe.radio || !(ap.rc_receiver_present || motors.armed())) {
|
|
g.rc_3.set_pwm(throttle_pwm);
|
|
return;
|
|
}
|
|
|
|
// check for 3 low throttle values
|
|
// Note: we do not pass through the low throttle until 3 low throttle values are recieved
|
|
failsafe.radio_counter++;
|
|
if( failsafe.radio_counter >= FS_COUNTER ) {
|
|
failsafe.radio_counter = FS_COUNTER; // check to ensure we don't overflow the counter
|
|
set_failsafe_radio(true);
|
|
g.rc_3.set_pwm(throttle_pwm); // pass through failsafe throttle
|
|
}
|
|
}else{
|
|
// we have a good throttle so reduce failsafe counter
|
|
failsafe.radio_counter--;
|
|
if( failsafe.radio_counter <= 0 ) {
|
|
failsafe.radio_counter = 0; // check to ensure we don't underflow the counter
|
|
|
|
// disengage failsafe after three (nearly) consecutive valid throttle values
|
|
if (failsafe.radio) {
|
|
set_failsafe_radio(false);
|
|
}
|
|
}
|
|
// pass through throttle
|
|
g.rc_3.set_pwm(throttle_pwm);
|
|
}
|
|
}
|
|
|
|
#define THROTTLE_ZERO_DEBOUNCE_TIME_MS 400
|
|
// set_throttle_zero_flag - set throttle_zero flag from debounced throttle control_in
|
|
static void set_throttle_zero_flag(int16_t throttle_control)
|
|
{
|
|
static uint32_t last_nonzero_throttle_ms = 0;
|
|
uint32_t tnow_ms = millis();
|
|
|
|
// if non-zero throttle immediately set as non-zero
|
|
if (throttle_control > 0) {
|
|
last_nonzero_throttle_ms = tnow_ms;
|
|
ap.throttle_zero = false;
|
|
} else if (tnow_ms - last_nonzero_throttle_ms > THROTTLE_ZERO_DEBOUNCE_TIME_MS) {
|
|
ap.throttle_zero = true;
|
|
}
|
|
}
|