ardupilot/APMrover2/radio.cpp
skyscraper 8c9e55edfa APMRover2: 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)
2016-05-10 16:21:16 +10:00

238 lines
7.0 KiB
C++

// -*- tab-width: 4; Mode: C++; c-basic-offset: 4; indent-tabs-mode: nil -*-
#include "Rover.h"
/*
allow for runtime change of control channel ordering
*/
void Rover::set_control_channels(void)
{
channel_steer = RC_Channel::rc_channel(rcmap.roll()-1);
channel_throttle = RC_Channel::rc_channel(rcmap.throttle()-1);
channel_learn = RC_Channel::rc_channel(g.learn_channel-1);
// set rc channel ranges
channel_steer->set_angle(SERVO_MAX);
channel_throttle->set_angle(100);
// For a rover safety is TRIM throttle
if (!arming.is_armed() && arming.arming_required() == AP_Arming::YES_MIN_PWM) {
hal.rcout->set_safety_pwm(1UL<<(rcmap.throttle()-1), channel_throttle->get_radio_trim());
}
// 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());
}
void Rover::init_rc_in()
{
// set rc dead zones
channel_steer->set_default_dead_zone(30);
channel_throttle->set_default_dead_zone(30);
//set auxiliary ranges
update_aux();
}
void Rover::init_rc_out()
{
RC_Channel::rc_channel(CH_1)->enable_out();
RC_Channel::rc_channel(CH_3)->enable_out();
if (arming.arming_required() != AP_Arming::YES_ZERO_PWM) {
channel_throttle->enable_out();
}
RC_Channel::output_trim_all();
// setup PWM values to send if the FMU firmware dies
RC_Channel::setup_failsafe_trim_all();
// output throttle trim when safety off if arming
// is setup for min on disarm. MIN is from plane where MIN is effectively no throttle.
// For Rover's no throttle means TRIM as rovers can go backwards i.e. MIN throttle is
// full speed backward.
if (arming.arming_required() == AP_Arming::YES_MIN_PWM) {
hal.rcout->set_safety_pwm(1UL<<(rcmap.throttle()-1), channel_throttle->get_radio_trim());
}
}
/*
check for driver input on rudder/steering stick for arming/disarming
*/
void Rover::rudder_arm_disarm_check()
{
// In Rover we need to check that its set to the throttle trim and within the DZ
// if throttle is not within trim dz, then pilot cannot rudder arm/disarm
if (!channel_throttle->in_trim_dz()) {
rudder_arm_timer = 0;
return;
}
// if not in a manual throttle mode then disallow rudder arming/disarming
if (auto_throttle_mode) {
rudder_arm_timer = 0;
return;
}
if (!arming.is_armed()) {
// when not armed, full right rudder starts arming counter
if (channel_steer->get_control_in() > 4000) {
uint32_t now = millis();
if (rudder_arm_timer == 0 ||
now - rudder_arm_timer < 3000) {
if (rudder_arm_timer == 0) {
rudder_arm_timer = now;
}
} else {
//time to arm!
arm_motors(AP_Arming::RUDDER);
rudder_arm_timer = 0;
}
} else {
// not at full right rudder
rudder_arm_timer = 0;
}
} else if (!motor_active()) {
// when armed and motor not active (not moving), full left rudder starts disarming counter
if (channel_steer->get_control_in() < -4000) {
uint32_t now = millis();
if (rudder_arm_timer == 0 ||
now - rudder_arm_timer < 3000) {
if (rudder_arm_timer == 0) {
rudder_arm_timer = now;
}
} else {
//time to disarm!
disarm_motors();
rudder_arm_timer = 0;
}
} else {
// not at full left rudder
rudder_arm_timer = 0;
}
}
}
void Rover::read_radio()
{
if (!hal.rcin->new_input()) {
control_failsafe(channel_throttle->get_radio_in());
return;
}
failsafe.last_valid_rc_ms = AP_HAL::millis();
RC_Channel::set_pwm_all();
control_failsafe(channel_throttle->get_radio_in());
channel_throttle->set_servo_out(channel_throttle->get_control_in());
// Check if the throttle value is above 50% and we need to nudge
// Make sure its above 50% in the direction we are travelling
if ((abs(channel_throttle->get_servo_out()) > 50) &&
(((channel_throttle->get_servo_out() < 0) && in_reverse) ||
((channel_throttle->get_servo_out() > 0) && !in_reverse))) {
throttle_nudge = (g.throttle_max - g.throttle_cruise) *
((fabsf(channel_throttle->norm_input())-0.5f) / 0.5f);
} else {
throttle_nudge = 0;
}
if (g.skid_steer_in) {
// convert the two radio_in values from skid steering values
/*
mixing rule:
steering = motor1 - motor2
throttle = 0.5*(motor1 + motor2)
motor1 = throttle + 0.5*steering
motor2 = throttle - 0.5*steering
*/
float motor1 = channel_steer->norm_input();
float motor2 = channel_throttle->norm_input();
float steering_scaled = motor1 - motor2;
float throttle_scaled = 0.5f*(motor1 + motor2);
int16_t steer = channel_steer->get_radio_trim();
int16_t thr = channel_throttle->get_radio_trim();
if (steering_scaled > 0.0f) {
steer += steering_scaled*(channel_steer->get_radio_max()-channel_steer->get_radio_trim());
} else {
steer += steering_scaled*(channel_steer->get_radio_trim()-channel_steer->get_radio_min());
}
if (throttle_scaled > 0.0f) {
thr += throttle_scaled*(channel_throttle->get_radio_max()-channel_throttle->get_radio_trim());
} else {
thr += throttle_scaled*(channel_throttle->get_radio_trim()-channel_throttle->get_radio_min());
}
channel_steer->set_pwm(steer);
channel_throttle->set_pwm(thr);
}
rudder_arm_disarm_check();
}
void Rover::control_failsafe(uint16_t pwm)
{
if (!g.fs_throttle_enabled) {
// no throttle failsafe
return;
}
// Check for failsafe condition based on loss of GCS control
if (rc_override_active) {
failsafe_trigger(FAILSAFE_EVENT_RC, (millis() - failsafe.rc_override_timer) > 1500);
} else if (g.fs_throttle_enabled) {
bool failed = pwm < (uint16_t)g.fs_throttle_value;
if (AP_HAL::millis() - failsafe.last_valid_rc_ms > 2000) {
failed = true;
}
failsafe_trigger(FAILSAFE_EVENT_THROTTLE, failed);
}
}
/*
return true if throttle level is below throttle failsafe threshold
or RC input is invalid
*/
bool Rover::throttle_failsafe_active(void)
{
if (!g.fs_throttle_enabled) {
return false;
}
if (millis() - failsafe.last_valid_rc_ms > 1000) {
// we haven't had a valid RC frame for 1 seconds
return true;
}
if (channel_throttle->get_reverse()) {
return channel_throttle->get_radio_in() >= g.fs_throttle_value;
}
return channel_throttle->get_radio_in() <= g.fs_throttle_value;
}
void Rover::trim_control_surfaces()
{
read_radio();
// Store control surface trim values
// ---------------------------------
if (channel_steer->get_radio_in() > 1400) {
channel_steer->set_radio_trim(channel_steer->get_radio_in());
// save to eeprom
channel_steer->save_eeprom();
}
}
void Rover::trim_radio()
{
for (int y = 0; y < 30; y++) {
read_radio();
}
trim_control_surfaces();
}