Ardupilot2/ArduCopter/motors.cpp
Andy Piper f84c855dd1 Copter: run copter attitude control with separate rate thread
run motors output at rate thread loop rate
allow rate thread to be enabled/disabled at runtime for in-flight impact testing
setup the right PID notch sample rate when using the rate thread the PID notches
 run at a very different sample rate
call update_dynamic_notch_at_specified_rate() in rate thread
log RTDT messages to track rate loop performance
set dt each cycle of the rate loop thread
run rate controller on samples as soon as they are ready
detect overload conditions in both the rate loop and main loop
decimate the rate thread if the CPU appears overloaded
decimate the gyro window inside the IMU
add in gyro drift to attitude rate thread
add fixed-rate thread option
configure rate loop based on AP_INERTIALSENSOR_FAST_SAMPLE_WINDOW_ENABLED
better rate loop thread decimation management
ensure fix rate attitude is enabled on arming
add rate loop timing debug
update backend filters rather than all the backends
provide more options around attitude rates
only log attitude and IMU from main loop
force trigger_groups() and reduce attitude thread priority
migrate fast rate enablement to FSTRATE_ENABLE
remove rate thread logging configuration and choose sensible logging rates
conditionally compile rate thread pieces
allow fast rate decimation to be user throttled
if target rate changes immediately jump to target rate
recover quickly from rate changes
ensure fixed rate always prints the rate on arming and is always up to date
add support for fixed rate attitude that does not change when disarmed
only push to subsystems at main loop rate
add logging and motor timing debug
correctly round gyro decimation rates
set dshot rate when changing attitude rate
fallback to higher dshot rates at lower loop rates
re-factor rate loop rate updates
log rates in systemid mode
reset target modifiers at loop rate
don't compile in support on tradheli
move rate thread into its own compilation unit
add rate loop config abstraction that allows code to be elided on non-copter builds
dynamically enable/disable rate thread correctly
add design comment for the rate thread

Co-authored-by: Andrew Tridgell <andrew@tridgell.net>
2024-12-04 07:45:05 +11:00

228 lines
7.5 KiB
C++

#include "Copter.h"
#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
#define LOST_VEHICLE_DELAY 10 // called at 10hz so 1 second
static uint32_t auto_disarm_begin;
// arm_motors_check - checks for pilot input to arm or disarm the copter
// called at 10hz
void Copter::arm_motors_check()
{
static int16_t arming_counter;
// check if arming/disarm using rudder is allowed
AP_Arming::RudderArming arming_rudder = arming.get_rudder_arming_type();
if (arming_rudder == AP_Arming::RudderArming::IS_DISABLED) {
arming_counter = 0;
return;
}
#if TOY_MODE_ENABLED
if (g2.toy_mode.enabled()) {
// not armed with sticks in toy mode
return;
}
#endif
// ensure throttle is down
if (channel_throttle->get_control_in() > 0) {
arming_counter = 0;
return;
}
int16_t yaw_in = channel_yaw->get_control_in();
// full right
if (yaw_in > 4000) {
// increase the arming counter to a maximum of 1 beyond the auto trim counter
if (arming_counter <= AUTO_TRIM_DELAY) {
arming_counter++;
}
// arm the motors and configure for flight
if (arming_counter == ARM_DELAY && !motors->armed()) {
// reset arming counter if arming fail
if (!arming.arm(AP_Arming::Method::RUDDER)) {
arming_counter = 0;
}
}
// arm the motors and configure for flight
if (arming_counter == AUTO_TRIM_DELAY && motors->armed() && flightmode->mode_number() == Mode::Number::STABILIZE) {
gcs().send_text(MAV_SEVERITY_INFO, "AutoTrim start");
auto_trim_counter = 250;
auto_trim_started = false;
// ensure auto-disarm doesn't trigger immediately
auto_disarm_begin = millis();
}
// full left and rudder disarming is enabled
} else if ((yaw_in < -4000) && (arming_rudder == AP_Arming::RudderArming::ARMDISARM)) {
if (!flightmode->has_manual_throttle() && !ap.land_complete) {
arming_counter = 0;
return;
}
// increase the counter to a maximum of 1 beyond the disarm delay
if (arming_counter <= DISARM_DELAY) {
arming_counter++;
}
// disarm the motors
if (arming_counter == DISARM_DELAY && motors->armed()) {
arming.disarm(AP_Arming::Method::RUDDER);
}
// Yaw is centered so reset arming counter
} else {
arming_counter = 0;
}
}
// 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
void Copter::auto_disarm_check()
{
uint32_t tnow_ms = millis();
uint32_t disarm_delay_ms = 1000*constrain_int16(g.disarm_delay, 0, 127);
// exit immediately if we are already disarmed, or if auto
// disarming is disabled
if (!motors->armed() || disarm_delay_ms == 0 || flightmode->mode_number() == Mode::Number::THROW) {
auto_disarm_begin = tnow_ms;
return;
}
// if the rotor is still spinning, don't initiate auto disarm
if (motors->get_spool_state() > AP_Motors::SpoolState::GROUND_IDLE) {
auto_disarm_begin = tnow_ms;
return;
}
// always allow auto disarm if using interlock switch or motors are Emergency Stopped
if ((ap.using_interlock && !motors->get_interlock()) || SRV_Channels::get_emergency_stop()) {
#if FRAME_CONFIG != HELI_FRAME
// use a shorter delay if using throttle interlock switch or Emergency Stop, because it is less
// obvious the copter is armed as the motors will not be spinning
disarm_delay_ms /= 2;
#endif
} else {
bool sprung_throttle_stick = (g.throttle_behavior & THR_BEHAVE_FEEDBACK_FROM_MID_STICK) != 0;
bool thr_low;
if (flightmode->has_manual_throttle() || !sprung_throttle_stick) {
thr_low = ap.throttle_zero;
} else {
float deadband_top = get_throttle_mid() + g.throttle_deadzone;
thr_low = channel_throttle->get_control_in() <= deadband_top;
}
if (!thr_low || !ap.land_complete) {
// reset timer
auto_disarm_begin = tnow_ms;
}
}
// disarm once timer expires
if ((tnow_ms-auto_disarm_begin) >= disarm_delay_ms) {
arming.disarm(AP_Arming::Method::DISARMDELAY);
auto_disarm_begin = tnow_ms;
}
}
// motors_output - send output to motors library which will adjust and send to ESCs and servos
void Copter::motors_output(bool full_push)
{
#if AP_COPTER_ADVANCED_FAILSAFE_ENABLED
// this is to allow the failsafe module to deliberately crash
// the vehicle. Only used in extreme circumstances to meet the
// OBC rules
if (g2.afs.should_crash_vehicle()) {
g2.afs.terminate_vehicle();
if (!g2.afs.terminating_vehicle_via_landing()) {
return;
}
// landing must continue to run the motors output
}
#endif
// Update arming delay state
if (ap.in_arming_delay && (!motors->armed() || millis()-arm_time_ms > ARMING_DELAY_SEC*1.0e3f || flightmode->mode_number() == Mode::Number::THROW)) {
ap.in_arming_delay = false;
}
// output any servo channels
SRV_Channels::calc_pwm();
auto &srv = AP::srv();
// cork now, so that all channel outputs happen at once
srv.cork();
// update output on any aux channels, for manual passthru
SRV_Channels::output_ch_all();
// 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);
LOGGER_WRITE_EVENT(LogEvent::MOTORS_INTERLOCK_ENABLED);
} else if (motors->get_interlock() && !interlock) {
motors->set_interlock(false);
LOGGER_WRITE_EVENT(LogEvent::MOTORS_INTERLOCK_DISABLED);
}
if (ap.motor_test) {
// check if we are performing the motor test
motor_test_output();
} else {
// send output signals to motors
flightmode->output_to_motors();
}
// push all channels
if (full_push) {
srv.push();
} else {
hal.rcout->push();
}
}
// motors_output from main thread
void Copter::motors_output_main()
{
if (!using_rate_thread) {
motors_output();
}
}
// check for pilot stick input to trigger lost vehicle alarm
void Copter::lost_vehicle_check()
{
static uint8_t soundalarm_counter;
// disable if aux switch is setup to vehicle alarm as the two could interfere
if (rc().find_channel_for_option(RC_Channel::AUX_FUNC::LOST_VEHICLE_SOUND)) {
return;
}
// ensure throttle is down, motors not armed, pitch and roll rc at max. Note: rc1=roll rc2=pitch
if (ap.throttle_zero && !motors->armed() && (channel_roll->get_control_in() > 4000) && (channel_pitch->get_control_in() > 4000)) {
if (soundalarm_counter >= LOST_VEHICLE_DELAY) {
if (AP_Notify::flags.vehicle_lost == false) {
AP_Notify::flags.vehicle_lost = true;
gcs().send_text(MAV_SEVERITY_NOTICE,"Locate Copter alarm");
}
} else {
soundalarm_counter++;
}
} else {
soundalarm_counter = 0;
if (AP_Notify::flags.vehicle_lost == true) {
AP_Notify::flags.vehicle_lost = false;
}
}
}