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ardupilot/libraries/SITL/SIM_FlightAxis.cpp

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/*
This program is free software: you can redistribute it and/or modify
it under the terms of the GNU General Public License as published by
the Free Software Foundation, either version 3 of the License, or
(at your option) any later version.
This program is distributed in the hope that it will be useful,
but WITHOUT ANY WARRANTY; without even the implied warranty of
MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the
GNU General Public License for more details.
You should have received a copy of the GNU General Public License
along with this program. If not, see <http://www.gnu.org/licenses/>.
*/
/*
simulator connector for FlightAxis
*/
#include "SIM_FlightAxis.h"
#include <arpa/inet.h>
#include <errno.h>
#include <fcntl.h>
#include <stdio.h>
#include <stdarg.h>
#include <sys/stat.h>
#include <sys/types.h>
#include <AP_HAL/AP_HAL.h>
#include <AP_Logger/AP_Logger.h>
#include "pthread.h"
extern const AP_HAL::HAL& hal;
using namespace SITL;
// the asprintf() calls are not worth checking for SITL
#pragma GCC diagnostic ignored "-Wunused-result"
static const struct {
const char *name;
float value;
bool save;
} sim_defaults[] = {
{ "BRD_OPTIONS", 0},
{ "AHRS_EKF_TYPE", 10 },
{ "INS_GYR_CAL", 0 },
{ "BATT_MONITOR", 4 },
{ "RC1_MIN", 1000, true },
{ "RC1_MAX", 2000, true },
{ "RC2_MIN", 1000, true },
{ "RC2_MAX", 2000, true },
{ "RC3_MIN", 1000, true },
{ "RC3_MAX", 2000, true },
{ "RC4_MIN", 1000, true },
{ "RC4_MAX", 2000, true },
{ "RC2_REVERSED", 1 }, // interlink has reversed rc2
{ "SERVO1_MIN", 1000 },
{ "SERVO1_MAX", 2000 },
{ "SERVO2_MIN", 1000 },
{ "SERVO2_MAX", 2000 },
{ "SERVO3_MIN", 1000 },
{ "SERVO3_MAX", 2000 },
{ "SERVO4_MIN", 1000 },
{ "SERVO4_MAX", 2000 },
{ "SERVO5_MIN", 1000 },
{ "SERVO5_MAX", 2000 },
{ "SERVO6_MIN", 1000 },
{ "SERVO6_MAX", 2000 },
{ "SERVO6_MIN", 1000 },
{ "SERVO6_MAX", 2000 },
{ "INS_ACC2OFFS_X", 0.001 },
{ "INS_ACC2OFFS_Y", 0.001 },
{ "INS_ACC2OFFS_Z", 0.001 },
{ "INS_ACC2SCAL_X", 1.001 },
{ "INS_ACC2SCAL_Y", 1.001 },
{ "INS_ACC2SCAL_Z", 1.001 },
{ "INS_ACCOFFS_X", 0.001 },
{ "INS_ACCOFFS_Y", 0.001 },
{ "INS_ACCOFFS_Z", 0.001 },
{ "INS_ACCSCAL_X", 1.001 },
{ "INS_ACCSCAL_Y", 1.001 },
{ "INS_ACCSCAL_Z", 1.001 },
};
FlightAxis::FlightAxis(const char *frame_str) :
Aircraft(frame_str)
{
use_time_sync = false;
num_motors = 2;
rate_hz = 250 / target_speedup;
heli_demix = strstr(frame_str, "helidemix") != nullptr;
rev4_servos = strstr(frame_str, "rev4") != nullptr;
const char *colon = strchr(frame_str, ':');
if (colon) {
controller_ip = colon+1;
}
for (uint8_t i=0; i<ARRAY_SIZE(sim_defaults); i++) {
AP_Param::set_default_by_name(sim_defaults[i].name, sim_defaults[i].value);
if (sim_defaults[i].save) {
enum ap_var_type ptype;
AP_Param *p = AP_Param::find(sim_defaults[i].name, &ptype);
if (!p->configured()) {
p->save();
}
}
}
int ret = pthread_create(&thread, NULL, update_thread, this);
if (ret != 0) {
AP_HAL::panic("SIM_FlightAxis: failed to create thread");
}
}
/*
update thread trampoline
*/
void *FlightAxis::update_thread(void *arg)
{
FlightAxis *flightaxis = (FlightAxis *)arg;
#if defined(__CYGWIN__) || defined(__CYGWIN64__)
//Cygwin doesn't support pthread_setname_np
#elif defined(__APPLE__) && defined(__MACH__)
pthread_setname_np("ardupilot-flightaxis");
#else
pthread_setname_np(pthread_self(), "ardupilot-flightaxis");
#endif
flightaxis->update_loop();
return nullptr;
}
/*
main update loop
*/
void FlightAxis::update_loop(void)
{
while (true) {
struct sitl_input new_input;
{
WITH_SEMAPHORE(mutex);
new_input = last_input;
}
exchange_data(new_input);
}
}
/*
extremely primitive SOAP parser that assumes the format used by FlightAxis
*/
void FlightAxis::parse_reply(const char *reply)
{
const char *reply0 = reply;
for (uint16_t i=0; i<num_keys; i++) {
const char *p = strstr(reply, keytable[i].key);
if (p == nullptr) {
p = strstr(reply0, keytable[i].key);
}
if (p == nullptr) {
printf("Failed to find key %s\n", keytable[i].key);
controller_started = false;
break;
}
p += strlen(keytable[i].key) + 1;
double v;
if (strncmp(p, "true", 4) == 0) {
v = 1;
} else if (strncmp(p, "false", 5) == 0) {
v = 0;
} else {
v = atof(p);
}
keytable[i].ref = v;
// this assumes key order and allows us to decode arrays
p = strchr(p, '>');
if (p != nullptr) {
reply = p;
}
}
}
/*
make a SOAP request, returning body of reply
*/
char *FlightAxis::soap_request(const char *action, const char *fmt, ...)
{
va_list ap;
char *req1;
va_start(ap, fmt);
vasprintf(&req1, fmt, ap);
va_end(ap);
//printf("%s\n", req1);
// open SOAP socket to FlightAxis
SocketAPM sock(false);
if (!sock.connect(controller_ip, controller_port)) {
free(req1);
return nullptr;
}
sock.set_blocking(false);
char *req;
asprintf(&req, R"(POST / HTTP/1.1
soapaction: '%s'
content-length: %u
content-type: text/xml;charset='UTF-8'
Connection: Keep-Alive
%s)",
action,
(unsigned)strlen(req1), req1);
sock.send(req, strlen(req));
free(req1);
free(req);
char reply[10000];
memset(reply, 0, sizeof(reply));
ssize_t ret = sock.recv(reply, sizeof(reply)-1, 1000);
if (ret <= 0) {
printf("No data\n");
return nullptr;
}
char *p = strstr(reply, "Content-Length: ");
if (p == nullptr) {
printf("No Content-Length\n");
return nullptr;
}
// get the content length
uint32_t content_length = strtoul(p+16, nullptr, 10);
char *body = strstr(p, "\r\n\r\n");
if (body == nullptr) {
printf("No body\n");
return nullptr;
}
body += 4;
// get the rest of the body
int32_t expected_length = content_length + (body - reply);
if (expected_length >= (int32_t)sizeof(reply)) {
printf("Reply too large %i\n", expected_length);
return nullptr;
}
while (ret < expected_length) {
ssize_t ret2 = sock.recv(&reply[ret], sizeof(reply)-(1+ret), 100);
if (ret2 <= 0) {
return nullptr;
}
// nul terminate
reply[ret+ret2] = 0;
ret += ret2;
}
return strdup(reply);
}
void FlightAxis::exchange_data(const struct sitl_input &input)
{
if (!controller_started ||
is_zero(state.m_flightAxisControllerIsActive) ||
!is_zero(state.m_resetButtonHasBeenPressed)) {
printf("Starting controller at %s\n", controller_ip);
// call a restore first. This allows us to connect after the aircraft is changed in RealFlight
char *reply = soap_request("RestoreOriginalControllerDevice", R"(<?xml version='1.0' encoding='UTF-8'?>
<soap:Envelope xmlns:soap='http://schemas.xmlsoap.org/soap/envelope/' xmlns:xsd='http://www.w3.org/2001/XMLSchema' xmlns:xsi='http://www.w3.org/2001/XMLSchema-instance'>
<soap:Body>
<RestoreOriginalControllerDevice><a>1</a><b>2</b></RestoreOriginalControllerDevice>
</soap:Body>
</soap:Envelope>)");
free(reply);
reply = soap_request("InjectUAVControllerInterface", R"(<?xml version='1.0' encoding='UTF-8'?>
<soap:Envelope xmlns:soap='http://schemas.xmlsoap.org/soap/envelope/' xmlns:xsd='http://www.w3.org/2001/XMLSchema' xmlns:xsi='http://www.w3.org/2001/XMLSchema-instance'>
<soap:Body>
<InjectUAVControllerInterface><a>1</a><b>2</b></InjectUAVControllerInterface>
</soap:Body>
</soap:Envelope>)");
free(reply);
activation_frame_counter = frame_counter;
controller_started = true;
}
// maximum number of servos to send is 12 with new FlightAxis
float scaled_servos[12];
for (uint8_t i=0; i<ARRAY_SIZE(scaled_servos); i++) {
scaled_servos[i] = (input.servos[i] - 1000) / 1000.0f;
}
if (rev4_servos) {
// swap first 4 and last 4 servos, for quadplane testing
float saved[4];
memcpy(saved, &scaled_servos[0], sizeof(saved));
memcpy(&scaled_servos[0], &scaled_servos[4], sizeof(saved));
memcpy(&scaled_servos[4], saved, sizeof(saved));
}
if (heli_demix) {
// FlightAxis expects "roll/pitch/collective/yaw" input
float swash1 = scaled_servos[0];
float swash2 = scaled_servos[1];
float swash3 = scaled_servos[2];
float roll_rate = swash1 - swash2;
float pitch_rate = -((swash1+swash2) / 2.0f - swash3);
scaled_servos[0] = constrain_float(roll_rate + 0.5, 0, 1);
scaled_servos[1] = constrain_float(pitch_rate + 0.5, 0, 1);
}
char *reply = soap_request("ExchangeData", R"(<?xml version='1.0' encoding='UTF-8'?><soap:Envelope xmlns:soap='http://schemas.xmlsoap.org/soap/envelope/' xmlns:xsd='http://www.w3.org/2001/XMLSchema' xmlns:xsi='http://www.w3.org/2001/XMLSchema-instance'>
<soap:Body>
<ExchangeData>
<pControlInputs>
<m-selectedChannels>4095</m-selectedChannels>
<m-channelValues-0to1>
<item>%.4f</item>
<item>%.4f</item>
<item>%.4f</item>
<item>%.4f</item>
<item>%.4f</item>
<item>%.4f</item>
<item>%.4f</item>
<item>%.4f</item>
<item>%.4f</item>
<item>%.4f</item>
<item>%.4f</item>
<item>%.4f</item>
</m-channelValues-0to1>
</pControlInputs>
</ExchangeData>
</soap:Body>
</soap:Envelope>)",
scaled_servos[0],
scaled_servos[1],
scaled_servos[2],
scaled_servos[3],
scaled_servos[4],
scaled_servos[5],
scaled_servos[6],
scaled_servos[7],
scaled_servos[8],
scaled_servos[9],
scaled_servos[10],
scaled_servos[11]);
if (reply) {
WITH_SEMAPHORE(mutex);
double lastt_s = state.m_currentPhysicsTime_SEC;
parse_reply(reply);
double dt = state.m_currentPhysicsTime_SEC - lastt_s;
if (dt > 0 && dt < 0.1) {
if (average_frame_time_s < 1.0e-6) {
average_frame_time_s = dt;
}
average_frame_time_s = average_frame_time_s * 0.98 + dt * 0.02;
}
socket_frame_counter++;
free(reply);
}
}
/*
update the FlightAxis simulation by one time step
*/
void FlightAxis::update(const struct sitl_input &input)
{
WITH_SEMAPHORE(mutex);
last_input = input;
double dt_seconds = state.m_currentPhysicsTime_SEC - last_time_s;
if (dt_seconds < 0) {
// cope with restarting RealFlight while connected
initial_time_s = time_now_us * 1.0e-6f;
last_time_s = state.m_currentPhysicsTime_SEC;
position_offset.zero();
return;
}
if (dt_seconds < 0.00001f) {
float delta_time = 0.001;
// don't go past the next expected frame
if (delta_time + extrapolated_s > average_frame_time_s) {
delta_time = average_frame_time_s - extrapolated_s;
}
if (delta_time <= 0) {
usleep(1000);
return;
}
time_now_us += delta_time * 1.0e6;
extrapolate_sensors(delta_time);
update_position();
update_mag_field_bf();
usleep(delta_time*1.0e6);
extrapolated_s += delta_time;
report_FPS();
return;
}
extrapolated_s = 0;
if (initial_time_s <= 0) {
dt_seconds = 0.001f;
initial_time_s = state.m_currentPhysicsTime_SEC - dt_seconds;
}
/*
the quaternion convention in realflight seems to have Z negative
*/
Quaternion quat(state.m_orientationQuaternion_W,
state.m_orientationQuaternion_Y,
state.m_orientationQuaternion_X,
-state.m_orientationQuaternion_Z);
quat.rotation_matrix(dcm);
gyro = Vector3f(radians(constrain_float(state.m_rollRate_DEGpSEC, -2000, 2000)),
radians(constrain_float(state.m_pitchRate_DEGpSEC, -2000, 2000)),
-radians(constrain_float(state.m_yawRate_DEGpSEC, -2000, 2000))) * target_speedup;
velocity_ef = Vector3f(state.m_velocityWorldU_MPS,
state.m_velocityWorldV_MPS,
state.m_velocityWorldW_MPS);
position = Vector3f(state.m_aircraftPositionY_MTR,
state.m_aircraftPositionX_MTR,
-state.m_altitudeASL_MTR - home.alt*0.01);
accel_body = {
float(state.m_accelerationBodyAX_MPS2),
float(state.m_accelerationBodyAY_MPS2),
float(state.m_accelerationBodyAZ_MPS2)
};
// accel on the ground is nasty in realflight, and prevents helicopter disarm
if (!is_zero(state.m_isTouchingGround)) {
Vector3f accel_ef = (velocity_ef - last_velocity_ef) / dt_seconds;
accel_ef.z -= GRAVITY_MSS;
accel_body = dcm.transposed() * accel_ef;
}
// limit to 16G to match pixhawk
float a_limit = GRAVITY_MSS*16;
accel_body.x = constrain_float(accel_body.x, -a_limit, a_limit);
accel_body.y = constrain_float(accel_body.y, -a_limit, a_limit);
accel_body.z = constrain_float(accel_body.z, -a_limit, a_limit);
// offset based on first position to account for offset in RF world
if (position_offset.is_zero() || !is_zero(state.m_resetButtonHasBeenPressed)) {
position_offset = position;
}
position -= position_offset;
airspeed = state.m_airspeed_MPS;
/* for pitot airspeed we need the airspeed along the X axis. We
can't get that from m_airspeed_MPS, so instead we calculate it
from wind vector and ground speed
*/
Vector3f m_wind_ef(-state.m_windY_MPS,-state.m_windX_MPS,-state.m_windZ_MPS);
Vector3f airspeed_3d_ef = m_wind_ef + velocity_ef;
Vector3f airspeed3d = dcm.mul_transpose(airspeed_3d_ef);
if (last_imu_rotation != ROTATION_NONE) {
airspeed3d = airspeed3d * sitl->ahrs_rotation_inv;
}
airspeed_pitot = MAX(airspeed3d.x,0);
#if 0
printf("WIND: %.1f %.1f %.1f AS3D %.1f %.1f %.1f\n",
state.m_windX_MPS,
state.m_windY_MPS,
state.m_windZ_MPS,
airspeed3d.x,
airspeed3d.y,
airspeed3d.z);
#endif
battery_voltage = state.m_batteryVoltage_VOLTS;
battery_current = state.m_batteryCurrentDraw_AMPS;
rpm[0] = state.m_heliMainRotorRPM;
rpm[1] = state.m_propRPM;
/*
the interlink interface supports 12 input channels
*/
rcin_chan_count = 12;
for (uint8_t i=0; i<rcin_chan_count; i++) {
rcin[i] = state.rcin[i];
}
update_position();
time_advance();
uint64_t new_time_us = (state.m_currentPhysicsTime_SEC - initial_time_s)*1.0e6;
if (new_time_us < time_now_us) {
uint64_t dt_us = time_now_us - new_time_us;
if (dt_us > 500000) {
// time going backwards
time_now_us = new_time_us;
}
} else {
time_now_us = new_time_us;
}
last_time_s = state.m_currentPhysicsTime_SEC;
last_velocity_ef = velocity_ef;
// update magnetic field
update_mag_field_bf();
report_FPS();
}
/*
report frame rates
*/
void FlightAxis::report_FPS(void)
{
if (frame_counter++ % 1000 == 0) {
if (!is_zero(last_frame_count_s)) {
uint64_t frames = socket_frame_counter - last_socket_frame_counter;
last_socket_frame_counter = socket_frame_counter;
double dt = state.m_currentPhysicsTime_SEC - last_frame_count_s;
printf("%.2f/%.2f FPS avg=%.2f\n",
frames / dt, 1000 / dt, 1.0/average_frame_time_s);
} else {
printf("Initial position %f %f %f\n", position.x, position.y, position.z);
}
last_frame_count_s = state.m_currentPhysicsTime_SEC;
}
}
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