ardupilot/ArduCopter/radio.cpp
Andrew Tridgell 2425c65e74 Copter: implement 'air-mode' for copter
this implements what betaflight calls 'air-mode'. This gives attitude
control when throttle is at zero, allowing for zero-throttle maneuvers,
plus keeping the copter level on the ground.

This was already implemented if an interlock switch was setup, but it
should also work with an arming switch. If using an arming switch then
throttle should not be considered zero as long as the arming switch
hasn't gone low.
2018-05-29 10:27:14 +09:00

212 lines
7.9 KiB
C++

#include "Copter.h"
// Function that will read the radio data, limit servos and trigger a failsafe
// ----------------------------------------------------------------------------
void Copter::default_dead_zones()
{
channel_roll->set_default_dead_zone(20);
channel_pitch->set_default_dead_zone(20);
#if FRAME_CONFIG == HELI_FRAME
channel_throttle->set_default_dead_zone(10);
channel_yaw->set_default_dead_zone(15);
RC_Channels::rc_channel(CH_6)->set_default_dead_zone(10);
#else
channel_throttle->set_default_dead_zone(30);
channel_yaw->set_default_dead_zone(20);
#endif
RC_Channels::rc_channel(CH_6)->set_default_dead_zone(0);
}
void Copter::init_rc_in()
{
channel_roll = RC_Channels::rc_channel(rcmap.roll()-1);
channel_pitch = RC_Channels::rc_channel(rcmap.pitch()-1);
channel_throttle = RC_Channels::rc_channel(rcmap.throttle()-1);
channel_yaw = RC_Channels::rc_channel(rcmap.yaw()-1);
// set rc channel ranges
channel_roll->set_angle(ROLL_PITCH_YAW_INPUT_MAX);
channel_pitch->set_angle(ROLL_PITCH_YAW_INPUT_MAX);
channel_yaw->set_angle(ROLL_PITCH_YAW_INPUT_MAX);
channel_throttle->set_range(1000);
//set auxiliary servo ranges
RC_Channels::rc_channel(CH_5)->set_range(1000);
RC_Channels::rc_channel(CH_6)->set_range(1000);
RC_Channels::rc_channel(CH_7)->set_range(1000);
RC_Channels::rc_channel(CH_8)->set_range(1000);
// set default dead zones
default_dead_zones();
// initialise throttle_zero flag
ap.throttle_zero = true;
// Allow override by default at start
ap.rc_override_enable = true;
}
// init_rc_out -- initialise motors and check if pilot wants to perform ESC calibration
void Copter::init_rc_out()
{
motors->set_loop_rate(scheduler.get_loop_rate_hz());
motors->init((AP_Motors::motor_frame_class)g2.frame_class.get(), (AP_Motors::motor_frame_type)g.frame_type.get());
// enable aux servos to cope with multiple output channels per motor
SRV_Channels::enable_aux_servos();
// update rate must be set after motors->init() to allow for motor mapping
motors->set_update_rate(g.rc_speed);
#if FRAME_CONFIG != HELI_FRAME
motors->set_throttle_range(channel_throttle->get_radio_min(), channel_throttle->get_radio_max());
#else
// setup correct scaling for ESCs like the UAVCAN PX4ESC which
// take a proportion of speed.
hal.rcout->set_esc_scaling(channel_throttle->get_radio_min(), channel_throttle->get_radio_max());
#endif
// refresh auxiliary channel to function map
SRV_Channels::update_aux_servo_function();
#if FRAME_CONFIG != HELI_FRAME
/*
setup a default safety ignore mask, so that servo gimbals can be active while safety is on
*/
uint16_t safety_ignore_mask = (~copter.motors->get_motor_mask()) & 0x3FFF;
BoardConfig.set_default_safety_ignore_mask(safety_ignore_mask);
#endif
// check if we should enter esc calibration mode
esc_calibration_startup_check();
}
// enable_motor_output() - enable and output lowest possible value to motors
void Copter::enable_motor_output()
{
// enable motors
motors->output_min();
}
void Copter::read_radio()
{
uint32_t tnow_ms = millis();
if (RC_Channels::read_input()) {
ap.new_radio_frame = true;
set_throttle_and_failsafe(channel_throttle->get_radio_in());
set_throttle_zero_flag(channel_throttle->get_control_in());
// flag we must have an rc receiver attached
if (!failsafe.rc_override_active) {
ap.rc_receiver_present = true;
}
// pass pilot input through to motors (used to allow wiggling servos while disarmed on heli, single, coax copters)
radio_passthrough_to_motors();
float dt = (tnow_ms - last_radio_update_ms)*1.0e-3f;
rc_throttle_control_in_filter.apply(channel_throttle->get_control_in(), dt);
last_radio_update_ms = tnow_ms;
}else{
uint32_t elapsed = tnow_ms - last_radio_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
void Copter::set_throttle_and_failsafe(uint16_t throttle_pwm)
{
// if failsafe not enabled pass through throttle and exit
if(g.failsafe_throttle == FS_THR_DISABLED) {
channel_throttle->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())) {
channel_throttle->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 received
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);
channel_throttle->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
channel_throttle->set_pwm(throttle_pwm);
}
}
#define THROTTLE_ZERO_DEBOUNCE_TIME_MS 400
// set_throttle_zero_flag - set throttle_zero flag from debounced throttle control
// throttle_zero is used to determine if the pilot intends to shut down the motors
// Basically, this signals when we are not flying. We are either on the ground
// or the pilot has shut down the copter in the air and it is free-falling
void Copter::set_throttle_zero_flag(int16_t throttle_control)
{
static uint32_t last_nonzero_throttle_ms = 0;
uint32_t tnow_ms = millis();
// if not using throttle interlock and non-zero throttle and not E-stopped,
// or using motor interlock and it's enabled, then motors are running,
// and we are flying. Immediately set as non-zero
if ((!ap.using_interlock && (throttle_control > 0) && !ap.motor_emergency_stop) ||
(ap.using_interlock && motors->get_interlock()) ||
ap.armed_with_switch) {
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;
}
}
// pass pilot's inputs to motors library (used to allow wiggling servos while disarmed on heli, single, coax copters)
void Copter::radio_passthrough_to_motors()
{
motors->set_radio_passthrough(channel_roll->norm_input(),
channel_pitch->norm_input(),
channel_throttle->get_control_in_zero_dz()*0.001,
channel_yaw->norm_input());
}
/*
return the throttle input for mid-stick as a control-in value
*/
int16_t Copter::get_throttle_mid(void)
{
#if TOY_MODE_ENABLED == ENABLED
if (g2.toy_mode.enabled()) {
return g2.toy_mode.get_throttle_mid();
}
#endif
return channel_throttle->get_control_mid();
}