2015-05-29 23:12:49 -03:00
|
|
|
#include "Copter.h"
|
|
|
|
|
2013-05-20 02:05:50 -03:00
|
|
|
#define ARM_DELAY 20 // called at 10hz so 2 seconds
|
|
|
|
#define DISARM_DELAY 20 // called at 10hz so 2 seconds
|
|
|
|
#define AUTO_TRIM_DELAY 100 // called at 10hz so 10 seconds
|
2015-04-28 11:06:39 -03:00
|
|
|
#define LOST_VEHICLE_DELAY 10 // called at 10hz so 1 second
|
2011-06-16 14:03:26 -03:00
|
|
|
|
2015-11-06 05:30:11 -04:00
|
|
|
static uint32_t auto_disarm_begin;
|
2014-10-09 10:42:47 -03:00
|
|
|
|
2013-05-20 01:03:18 -03:00
|
|
|
// arm_motors_check - checks for pilot input to arm or disarm the copter
|
2011-06-16 14:03:26 -03:00
|
|
|
// called at 10hz
|
2015-05-29 23:12:49 -03:00
|
|
|
void Copter::arm_motors_check()
|
2011-01-23 22:04:44 -04:00
|
|
|
{
|
2012-08-21 23:19:50 -03:00
|
|
|
static int16_t arming_counter;
|
|
|
|
|
2018-09-09 21:19:49 -03:00
|
|
|
// check if arming/disarm using rudder is allowed
|
2019-03-06 23:12:50 -04:00
|
|
|
AP_Arming::RudderArming arming_rudder = arming.get_rudder_arming_type();
|
|
|
|
if (arming_rudder == AP_Arming::RudderArming::IS_DISABLED) {
|
2024-06-02 04:41:28 -03:00
|
|
|
arming_counter = 0;
|
2018-09-09 21:19:49 -03:00
|
|
|
return;
|
|
|
|
}
|
|
|
|
|
2024-09-04 00:48:37 -03:00
|
|
|
#if TOY_MODE_ENABLED
|
2018-01-18 02:49:20 -04:00
|
|
|
if (g2.toy_mode.enabled()) {
|
|
|
|
// not armed with sticks in toy mode
|
|
|
|
return;
|
|
|
|
}
|
|
|
|
#endif
|
2018-09-09 21:21:31 -03:00
|
|
|
|
2013-05-16 04:32:00 -03:00
|
|
|
// ensure throttle is down
|
ArduCopter: Fix up after refactoring RC_Channel class
Further to refactor of RC_Channel class which included
adding get_xx set_xx methods, change reads and writes to the public members
to calls to get and set functionsss
old public member(int16_t) get function -> int16_t set function (int16_t)
(expression where c is an object of type RC_Channel)
c.radio_in c.get_radio_in() c.set_radio_in(v)
c.control_in c.get_control_in() c.set_control_in(v)
c.servo_out c.get_servo_out() c.set_servo_out(v)
c.pwm_out c.get_pwm_out() // use existing
c.radio_out c.get_radio_out() c.set_radio_out(v)
c.radio_max c.get_radio_max() c.set_radio_max(v)
c.radio_min c.get_radio_min() c.set_radio_min(v)
c.radio_trim c.get_radio_trim() c.set_radio_trim(v);
c.min_max_configured() // return true if min and max are configured
Because data members of RC_Channels are now private and so cannot be written directly
some overloads are provided in the Plane classes to provide the old functionality
new overload Plane::stick_mix_channel(RC_Channel *channel)
which forwards to the previously existing
void stick_mix_channel(RC_Channel *channel, int16_t &servo_out);
new overload Plane::channel_output_mixer(Rc_Channel* , RC_Channel*)const
which forwards to
(uint8_t mixing_type, int16_t & chan1, int16_t & chan2)const;
Rename functions
RC_Channel_aux::set_radio_trim(Aux_servo_function_t function)
to RC_Channel_aux::set_trim_to_radio_in_for(Aux_servo_function_t function)
RC_Channel_aux::set_servo_out(Aux_servo_function_t function, int16_t value)
to RC_Channel_aux::set_servo_out_for(Aux_servo_function_t function, int16_t value)
Rationale:
RC_Channel is a complicated class, which combines
several functionalities dealing with stick inputs
in pwm and logical units, logical and actual actuator
outputs, unit conversion etc, etc
The intent of this PR is to clarify existing use of
the class. At the basic level it should now be possible
to grep all places where private variable is set by
searching for the set_xx function.
(The wider purpose is to provide a more generic and
logically simpler method of output mixing. This is a small step)
2016-05-08 05:46:59 -03:00
|
|
|
if (channel_throttle->get_control_in() > 0) {
|
2012-08-21 23:19:50 -03:00
|
|
|
arming_counter = 0;
|
|
|
|
return;
|
|
|
|
}
|
|
|
|
|
2018-09-09 21:21:31 -03:00
|
|
|
int16_t yaw_in = channel_yaw->get_control_in();
|
2012-08-21 23:19:50 -03:00
|
|
|
|
|
|
|
// full right
|
2018-09-09 21:21:31 -03:00
|
|
|
if (yaw_in > 4000) {
|
2012-07-14 23:26:17 -03:00
|
|
|
|
2012-12-19 11:06:20 -04:00
|
|
|
// increase the arming counter to a maximum of 1 beyond the auto trim counter
|
2018-09-09 21:21:31 -03:00
|
|
|
if (arming_counter <= AUTO_TRIM_DELAY) {
|
2012-12-19 11:06:20 -04:00
|
|
|
arming_counter++;
|
|
|
|
}
|
|
|
|
|
|
|
|
// arm the motors and configure for flight
|
2017-01-09 03:31:26 -04:00
|
|
|
if (arming_counter == ARM_DELAY && !motors->armed()) {
|
2015-01-30 04:56:22 -04:00
|
|
|
// reset arming counter if arming fail
|
2019-05-05 22:39:57 -03:00
|
|
|
if (!arming.arm(AP_Arming::Method::RUDDER)) {
|
2013-05-20 01:03:18 -03:00
|
|
|
arming_counter = 0;
|
|
|
|
}
|
2012-12-19 11:06:20 -04:00
|
|
|
}
|
2012-07-14 23:26:17 -03:00
|
|
|
|
2012-12-19 11:06:20 -04:00
|
|
|
// arm the motors and configure for flight
|
2020-01-30 03:29:36 -04:00
|
|
|
if (arming_counter == AUTO_TRIM_DELAY && motors->armed() && flightmode->mode_number() == Mode::Number::STABILIZE) {
|
2020-06-03 00:28:04 -03:00
|
|
|
gcs().send_text(MAV_SEVERITY_INFO, "AutoTrim start");
|
2012-12-19 11:06:20 -04:00
|
|
|
auto_trim_counter = 250;
|
2020-06-03 00:28:04 -03:00
|
|
|
auto_trim_started = false;
|
2014-10-09 10:42:47 -03:00
|
|
|
// ensure auto-disarm doesn't trigger immediately
|
2015-11-06 05:30:11 -04:00
|
|
|
auto_disarm_begin = millis();
|
2012-08-21 23:19:50 -03:00
|
|
|
}
|
|
|
|
|
2018-09-09 21:19:49 -03:00
|
|
|
// full left and rudder disarming is enabled
|
2019-03-06 23:12:50 -04:00
|
|
|
} else if ((yaw_in < -4000) && (arming_rudder == AP_Arming::RudderArming::ARMDISARM)) {
|
2017-12-05 19:56:38 -04:00
|
|
|
if (!flightmode->has_manual_throttle() && !ap.land_complete) {
|
2014-10-10 06:29:10 -03:00
|
|
|
arming_counter = 0;
|
|
|
|
return;
|
|
|
|
}
|
2012-12-19 11:06:20 -04:00
|
|
|
|
|
|
|
// increase the counter to a maximum of 1 beyond the disarm delay
|
2018-09-09 21:21:31 -03:00
|
|
|
if (arming_counter <= DISARM_DELAY) {
|
2012-08-21 23:19:50 -03:00
|
|
|
arming_counter++;
|
|
|
|
}
|
|
|
|
|
2012-12-19 11:06:20 -04:00
|
|
|
// disarm the motors
|
2017-01-09 03:31:26 -04:00
|
|
|
if (arming_counter == DISARM_DELAY && motors->armed()) {
|
2020-02-21 09:09:57 -04:00
|
|
|
arming.disarm(AP_Arming::Method::RUDDER);
|
2012-12-19 11:06:20 -04:00
|
|
|
}
|
|
|
|
|
|
|
|
// Yaw is centered so reset arming counter
|
2018-09-09 21:21:31 -03:00
|
|
|
} else {
|
2012-08-21 23:19:50 -03:00
|
|
|
arming_counter = 0;
|
|
|
|
}
|
2011-01-23 22:04:44 -04:00
|
|
|
}
|
|
|
|
|
2013-11-18 03:13:15 -04:00
|
|
|
// auto_disarm_check - disarms the copter if it has been sitting on the ground in manual mode with throttle low for at least 15 seconds
|
2015-05-29 23:12:49 -03:00
|
|
|
void Copter::auto_disarm_check()
|
2013-05-20 02:05:50 -03:00
|
|
|
{
|
2015-11-06 05:30:11 -04:00
|
|
|
uint32_t tnow_ms = millis();
|
|
|
|
uint32_t disarm_delay_ms = 1000*constrain_int16(g.disarm_delay, 0, 127);
|
2015-03-13 15:33:19 -03:00
|
|
|
|
2015-08-30 22:44:08 -03:00
|
|
|
// exit immediately if we are already disarmed, or if auto
|
|
|
|
// disarming is disabled
|
2020-01-30 03:29:36 -04:00
|
|
|
if (!motors->armed() || disarm_delay_ms == 0 || flightmode->mode_number() == Mode::Number::THROW) {
|
2015-11-06 05:30:11 -04:00
|
|
|
auto_disarm_begin = tnow_ms;
|
2013-11-18 03:13:15 -04:00
|
|
|
return;
|
|
|
|
}
|
|
|
|
|
2015-11-06 18:36:56 -04:00
|
|
|
// if the rotor is still spinning, don't initiate auto disarm
|
2019-04-12 01:53:34 -03:00
|
|
|
if (motors->get_spool_state() > AP_Motors::SpoolState::GROUND_IDLE) {
|
2015-11-13 20:59:59 -04:00
|
|
|
auto_disarm_begin = tnow_ms;
|
2015-11-06 18:36:56 -04:00
|
|
|
return;
|
|
|
|
}
|
|
|
|
|
2015-04-22 14:56:05 -03:00
|
|
|
// always allow auto disarm if using interlock switch or motors are Emergency Stopped
|
2019-01-25 14:57:36 -04:00
|
|
|
if ((ap.using_interlock && !motors->get_interlock()) || SRV_Channels::get_emergency_stop()) {
|
2015-08-02 22:17:53 -03:00
|
|
|
#if FRAME_CONFIG != HELI_FRAME
|
2015-04-22 14:56:05 -03:00
|
|
|
// use a shorter delay if using throttle interlock switch or Emergency Stop, because it is less
|
2015-03-13 15:33:19 -03:00
|
|
|
// obvious the copter is armed as the motors will not be spinning
|
2015-11-06 05:30:11 -04:00
|
|
|
disarm_delay_ms /= 2;
|
2015-08-02 22:17:53 -03:00
|
|
|
#endif
|
2015-08-14 16:08:03 -03:00
|
|
|
} else {
|
|
|
|
bool sprung_throttle_stick = (g.throttle_behavior & THR_BEHAVE_FEEDBACK_FROM_MID_STICK) != 0;
|
|
|
|
bool thr_low;
|
2017-12-05 19:56:38 -04:00
|
|
|
if (flightmode->has_manual_throttle() || !sprung_throttle_stick) {
|
2015-08-14 16:08:03 -03:00
|
|
|
thr_low = ap.throttle_zero;
|
2015-03-13 15:33:19 -03:00
|
|
|
} else {
|
2018-01-18 02:49:20 -04:00
|
|
|
float deadband_top = get_throttle_mid() + g.throttle_deadzone;
|
2017-01-06 21:06:40 -04:00
|
|
|
thr_low = channel_throttle->get_control_in() <= deadband_top;
|
2015-03-13 15:33:19 -03:00
|
|
|
}
|
|
|
|
|
2015-11-06 05:30:11 -04:00
|
|
|
if (!thr_low || !ap.land_complete) {
|
|
|
|
// reset timer
|
|
|
|
auto_disarm_begin = tnow_ms;
|
2013-05-20 02:05:50 -03:00
|
|
|
}
|
2015-08-14 16:08:03 -03:00
|
|
|
}
|
|
|
|
|
2015-11-06 05:30:11 -04:00
|
|
|
// disarm once timer expires
|
|
|
|
if ((tnow_ms-auto_disarm_begin) >= disarm_delay_ms) {
|
2020-02-21 09:09:57 -04:00
|
|
|
arming.disarm(AP_Arming::Method::DISARMDELAY);
|
2015-11-06 05:30:11 -04:00
|
|
|
auto_disarm_begin = tnow_ms;
|
2013-05-20 02:05:50 -03:00
|
|
|
}
|
|
|
|
}
|
2011-01-23 22:04:44 -04:00
|
|
|
|
2015-01-21 07:20:05 -04:00
|
|
|
// motors_output - send output to motors library which will adjust and send to ESCs and servos
|
2024-10-25 01:04:08 -03:00
|
|
|
// full_push is true when slower rate updates (e.g. servo output) need to be performed at the main loop rate.
|
2024-02-11 01:19:56 -04:00
|
|
|
void Copter::motors_output(bool full_push)
|
2011-01-23 22:04:44 -04:00
|
|
|
{
|
2024-11-06 04:09:47 -04:00
|
|
|
#if AP_COPTER_ADVANCED_FAILSAFE_ENABLED
|
2017-07-31 02:21:40 -03:00
|
|
|
// this is to allow the failsafe module to deliberately crash
|
2016-08-16 07:23:27 -03:00
|
|
|
// the vehicle. Only used in extreme circumstances to meet the
|
|
|
|
// OBC rules
|
|
|
|
if (g2.afs.should_crash_vehicle()) {
|
|
|
|
g2.afs.terminate_vehicle();
|
2018-09-29 04:34:36 -03:00
|
|
|
if (!g2.afs.terminating_vehicle_via_landing()) {
|
|
|
|
return;
|
|
|
|
}
|
|
|
|
// landing must continue to run the motors output
|
2016-08-16 07:23:27 -03:00
|
|
|
}
|
|
|
|
#endif
|
|
|
|
|
2016-01-21 22:59:47 -04:00
|
|
|
// Update arming delay state
|
2020-01-30 03:29:36 -04:00
|
|
|
if (ap.in_arming_delay && (!motors->armed() || millis()-arm_time_ms > ARMING_DELAY_SEC*1.0e3f || flightmode->mode_number() == Mode::Number::THROW)) {
|
2016-01-21 22:59:47 -04:00
|
|
|
ap.in_arming_delay = false;
|
|
|
|
}
|
|
|
|
|
2017-04-17 03:32:34 -03:00
|
|
|
// output any servo channels
|
|
|
|
SRV_Channels::calc_pwm();
|
2017-04-17 20:40:49 -03:00
|
|
|
|
2024-11-12 17:09:59 -04:00
|
|
|
auto &srv = AP::srv();
|
|
|
|
|
2017-04-17 20:40:49 -03:00
|
|
|
// cork now, so that all channel outputs happen at once
|
2024-11-12 17:09:59 -04:00
|
|
|
srv.cork();
|
2017-07-31 02:21:40 -03:00
|
|
|
|
2017-04-17 20:40:49 -03:00
|
|
|
// update output on any aux channels, for manual passthru
|
|
|
|
SRV_Channels::output_ch_all();
|
2017-07-31 02:21:40 -03:00
|
|
|
|
2022-01-27 11:36:37 -04:00
|
|
|
// update motors interlock state
|
|
|
|
bool interlock = motors->armed() && !ap.in_arming_delay && (!ap.using_interlock || ap.motor_interlock_switch) && !SRV_Channels::get_emergency_stop();
|
|
|
|
if (!motors->get_interlock() && interlock) {
|
|
|
|
motors->set_interlock(true);
|
2023-07-13 21:58:09 -03:00
|
|
|
LOGGER_WRITE_EVENT(LogEvent::MOTORS_INTERLOCK_ENABLED);
|
2022-01-27 11:36:37 -04:00
|
|
|
} else if (motors->get_interlock() && !interlock) {
|
|
|
|
motors->set_interlock(false);
|
2023-07-13 21:58:09 -03:00
|
|
|
LOGGER_WRITE_EVENT(LogEvent::MOTORS_INTERLOCK_DISABLED);
|
2022-01-27 11:36:37 -04:00
|
|
|
}
|
|
|
|
|
2014-04-28 04:27:27 -03:00
|
|
|
if (ap.motor_test) {
|
2022-01-27 11:36:37 -04:00
|
|
|
// check if we are performing the motor test
|
2014-04-28 04:27:27 -03:00
|
|
|
motor_test_output();
|
|
|
|
} else {
|
2016-01-21 22:59:47 -04:00
|
|
|
// send output signals to motors
|
2021-08-14 06:12:18 -03:00
|
|
|
flightmode->output_to_motors();
|
2014-04-28 04:27:27 -03:00
|
|
|
}
|
2017-04-17 20:40:49 -03:00
|
|
|
|
|
|
|
// push all channels
|
2024-02-11 01:19:56 -04:00
|
|
|
if (full_push) {
|
2024-10-25 01:04:08 -03:00
|
|
|
// motor output including servos and other updates that need to run at the main loop rate
|
2024-02-11 01:19:56 -04:00
|
|
|
srv.push();
|
|
|
|
} else {
|
2024-10-25 01:04:08 -03:00
|
|
|
// motor output only at main loop rate or faster
|
2024-02-11 01:19:56 -04:00
|
|
|
hal.rcout->push();
|
|
|
|
}
|
|
|
|
}
|
|
|
|
|
2024-10-25 01:04:08 -03:00
|
|
|
// motors_output from main thread at main loop rate
|
2024-02-11 01:19:56 -04:00
|
|
|
void Copter::motors_output_main()
|
|
|
|
{
|
|
|
|
if (!using_rate_thread) {
|
|
|
|
motors_output();
|
|
|
|
}
|
2012-01-01 16:46:32 -04:00
|
|
|
}
|
2015-04-28 11:06:39 -03:00
|
|
|
|
|
|
|
// check for pilot stick input to trigger lost vehicle alarm
|
2015-05-29 23:12:49 -03:00
|
|
|
void Copter::lost_vehicle_check()
|
2015-04-28 11:06:39 -03:00
|
|
|
{
|
|
|
|
static uint8_t soundalarm_counter;
|
|
|
|
|
|
|
|
// disable if aux switch is setup to vehicle alarm as the two could interfere
|
2019-04-03 13:25:47 -03:00
|
|
|
if (rc().find_channel_for_option(RC_Channel::AUX_FUNC::LOST_VEHICLE_SOUND)) {
|
2015-04-28 11:06:39 -03:00
|
|
|
return;
|
|
|
|
}
|
|
|
|
|
|
|
|
// ensure throttle is down, motors not armed, pitch and roll rc at max. Note: rc1=roll rc2=pitch
|
2017-01-09 03:31:26 -04:00
|
|
|
if (ap.throttle_zero && !motors->armed() && (channel_roll->get_control_in() > 4000) && (channel_pitch->get_control_in() > 4000)) {
|
2015-04-28 11:06:39 -03:00
|
|
|
if (soundalarm_counter >= LOST_VEHICLE_DELAY) {
|
|
|
|
if (AP_Notify::flags.vehicle_lost == false) {
|
|
|
|
AP_Notify::flags.vehicle_lost = true;
|
2017-07-08 21:56:49 -03:00
|
|
|
gcs().send_text(MAV_SEVERITY_NOTICE,"Locate Copter alarm");
|
2015-04-28 11:06:39 -03:00
|
|
|
}
|
|
|
|
} else {
|
|
|
|
soundalarm_counter++;
|
|
|
|
}
|
|
|
|
} else {
|
|
|
|
soundalarm_counter = 0;
|
|
|
|
if (AP_Notify::flags.vehicle_lost == true) {
|
|
|
|
AP_Notify::flags.vehicle_lost = false;
|
|
|
|
}
|
|
|
|
}
|
|
|
|
}
|