2015-05-10 08:01:49 -03:00
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/// -*- tab-width: 4; Mode: C++; c-basic-offset: 4; indent-tabs-mode: nil -*-
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/*
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This program is free software: you can redistribute it and/or modify
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it under the terms of the GNU General Public License as published by
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the Free Software Foundation, either version 3 of the License, or
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(at your option) any later version.
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This program is distributed in the hope that it will be useful,
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but WITHOUT ANY WARRANTY; without even the implied warranty of
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MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the
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GNU General Public License for more details.
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You should have received a copy of the GNU General Public License
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along with this program. If not, see <http://www.gnu.org/licenses/>.
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*/
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/*
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simulator connector for ardupilot version of JSBSim
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*/
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#include <AP_HAL.h>
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#if CONFIG_HAL_BOARD == HAL_BOARD_SITL
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#include "SIM_JSBSim.h"
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#include <stdio.h>
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#include <sys/types.h>
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#include <sys/stat.h>
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#include <fcntl.h>
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#include <arpa/inet.h>
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2015-05-21 19:04:38 -03:00
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#include <errno.h>
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2015-05-10 08:01:49 -03:00
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extern const AP_HAL::HAL& hal;
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2015-05-10 08:57:39 -03:00
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// the asprintf() calls are not worth checking for SITL
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2015-05-10 08:01:49 -03:00
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#pragma GCC diagnostic ignored "-Wunused-result"
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2015-05-10 08:57:39 -03:00
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#define DEBUG_JSBSIM 1
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#define FEET_TO_METERS 0.3048f
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2015-05-10 08:01:49 -03:00
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/*
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constructor
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*/
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JSBSim::JSBSim(const char *home_str, const char *frame_str) :
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Aircraft(home_str, frame_str),
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sock_control(false),
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sock_fgfdm(true),
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initialised(false),
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jsbsim_script(NULL),
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jsbsim_fgout(NULL),
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created_templates(false),
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started_jsbsim(false),
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opened_control_socket(false),
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opened_fdm_socket(false),
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frame(FRAME_NORMAL)
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{
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if (strstr(frame_str, "elevon")) {
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frame = FRAME_ELEVON;
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} else if (strstr(frame_str, "vtail")) {
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frame = FRAME_VTAIL;
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} else {
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frame = FRAME_NORMAL;
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}
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2015-05-10 08:01:49 -03:00
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}
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/*
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create template files
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*/
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bool JSBSim::create_templates(void)
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{
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if (created_templates) {
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return true;
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}
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control_port = 5505 + instance*10;
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fdm_port = 5504 + instance*10;
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asprintf(&jsbsim_script, "%s/jsbsim_start_%u.xml", autotest_dir, instance);
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asprintf(&jsbsim_fgout, "%s/jsbsim_fgout_%u.xml", autotest_dir, instance);
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FILE *f = fopen(jsbsim_script, "w");
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if (f == NULL) {
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hal.scheduler->panic("Unable to create jsbsim script");
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}
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fprintf(f,
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"<?xml version=\"1.0\" encoding=\"utf-8\"?>\n"
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"<?xml-stylesheet type=\"text/xsl\" href=\"http://jsbsim.sf.net/JSBSimScript.xsl\"?>\n"
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"<runscript xmlns:xsi=\"http://www.w3.org/2001/XMLSchema-instance\"\n"
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" xsi:noNamespaceSchemaLocation=\"http://jsbsim.sf.net/JSBSimScript.xsd\"\n"
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" name=\"Testing Rascal110\">\n"
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"\n"
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" <description>\n"
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" test ArduPlane using Rascal110 and JSBSim\n"
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" </description>\n"
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"\n"
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" <use aircraft=\"Rascal\" initialize=\"reset\"/>\n"
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"\n"
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" <!-- we control the servos via the jsbsim console\n"
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" interface on TCP 5124 -->\n"
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" <input port=\"%u\"/>\n"
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"\n"
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" <run start=\"0\" end=\"10000000\" dt=\"0.001\">\n"
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" <property value=\"0\"> simulation/notify-time-trigger </property>\n"
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"\n"
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" <event name=\"start engine\">\n"
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" <condition> simulation/sim-time-sec le 0.01 </condition>\n"
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" <set name=\"propulsion/engine[0]/set-running\" value=\"1\"/>\n"
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" <notify/>\n"
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" </event>\n"
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"\n"
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" <event name=\"Trim\">\n"
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" <condition>simulation/sim-time-sec ge 0.01</condition>\n"
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" <set name=\"simulation/do_simple_trim\" value=\"2\"/>\n"
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" <notify/>\n"
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" </event>\n"
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" </run>\n"
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"\n"
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"</runscript>\n"
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"", control_port);
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fclose(f);
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f = fopen(jsbsim_fgout, "w");
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if (f == NULL) {
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hal.scheduler->panic("Unable to create jsbsim fgout script");
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}
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fprintf(f, "<?xml version=\"1.0\"?>\n"
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"<output name=\"127.0.0.1\" type=\"FLIGHTGEAR\" port=\"%u\" protocol=\"udp\" rate=\"1000\"/>\n",
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fdm_port);
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fclose(f);
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2015-05-10 08:57:39 -03:00
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char *jsbsim_reset;
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asprintf(&jsbsim_reset, "%s/aircraft/Rascal/reset.xml", autotest_dir);
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f = fopen(jsbsim_reset, "w");
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if (f == NULL) {
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hal.scheduler->panic("Unable to create jsbsim Rascal reset script");
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}
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float r, p, y;
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dcm.to_euler(&r, &p, &y);
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fprintf(f,
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"<?xml version=\"1.0\"?>\n"
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"<initialize name=\"Start up location\">\n"
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" <latitude unit=\"DEG\"> %f </latitude>\n"
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" <longitude unit=\"DEG\"> %f </longitude>\n"
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" <altitude unit=\"M\"> 1.3 </altitude>\n"
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" <vt unit=\"FT/SEC\"> 0.0 </vt>\n"
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" <gamma unit=\"DEG\"> 0.0 </gamma>\n"
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" <phi unit=\"DEG\"> 0.0 </phi>\n"
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" <theta unit=\"DEG\"> 13.0 </theta>\n"
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" <psi unit=\"DEG\"> %f </psi>\n"
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"</initialize>\n",
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home.lat*1.0e-7,
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home.lng*1.0e-7,
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degrees(y));
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fclose(f);
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2015-05-10 08:01:49 -03:00
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created_templates = true;
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return true;
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}
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/*
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start JSBSim child
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*/
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bool JSBSim::start_JSBSim(void)
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{
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if (started_jsbsim) {
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return true;
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}
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if (!open_fdm_socket()) {
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return false;
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}
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int p[2];
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int devnull = open("/dev/null", O_RDWR);
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if (pipe(p) != 0) {
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hal.scheduler->panic("Unable to create pipe");
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}
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pid_t child_pid = fork();
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if (child_pid == 0) {
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// in child
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dup2(devnull, 0);
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dup2(p[1], 1);
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close(p[0]);
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for (uint8_t i=3; i<100; i++) {
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close(i);
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}
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char *logdirective;
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char *script;
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asprintf(&logdirective, "--logdirectivefile=%s", jsbsim_fgout);
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asprintf(&script, "--script=%s", jsbsim_script);
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if (chdir(autotest_dir) != 0) {
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perror(autotest_dir);
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exit(1);
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}
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int ret = execlp("JSBSim",
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"JSBSim",
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"--realtime",
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"--suspend",
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"--nice",
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"--simulation-rate=1000",
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logdirective,
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script,
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NULL);
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if (ret != 0) {
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perror("JSBSim");
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}
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exit(1);
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}
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close(p[1]);
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jsbsim_stdout = p[0];
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// read startup to be sure it is running
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char c;
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if (read(jsbsim_stdout, &c, 1) != 1) {
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hal.scheduler->panic("Unable to start JSBSim");
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}
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if (!expect("JSBSim Execution beginning")) {
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hal.scheduler->panic("Failed to start JSBSim");
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}
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if (!open_control_socket()) {
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hal.scheduler->panic("Failed to open JSBSim control socket");
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}
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fcntl(jsbsim_stdout, F_SETFL, fcntl(jsbsim_stdout, F_GETFL, 0) | O_NONBLOCK);
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started_jsbsim = true;
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check_stdout();
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return true;
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}
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/*
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check for stdout from JSBSim
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*/
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void JSBSim::check_stdout(void)
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{
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char line[100];
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ssize_t ret = ::read(jsbsim_stdout, line, sizeof(line));
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if (ret > 0) {
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#if DEBUG_JSBSIM
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write(1, line, ret);
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#endif
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}
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}
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/*
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a simple function to wait for a string on jsbsim_stdout
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*/
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bool JSBSim::expect(const char *str)
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{
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const char *basestr = str;
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while (*str) {
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char c;
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if (read(jsbsim_stdout, &c, 1) != 1) {
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return false;
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}
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if (c == *str) {
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str++;
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} else {
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str = basestr;
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}
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#if DEBUG_JSBSIM
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write(1, &c, 1);
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#endif
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}
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return true;
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}
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/*
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open control socket to JSBSim
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*/
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bool JSBSim::open_control_socket(void)
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{
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if (opened_control_socket) {
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return true;
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}
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if (!sock_control.connect("127.0.0.1", control_port)) {
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return false;
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}
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printf("Opened JSBSim control socket\n");
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sock_control.set_blocking(false);
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opened_control_socket = true;
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char startup[] = "info\nresume\nstep\n";
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sock_control.send(startup, strlen(startup));
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return true;
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}
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/*
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open fdm socket from JSBSim
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*/
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bool JSBSim::open_fdm_socket(void)
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{
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if (opened_fdm_socket) {
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return true;
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}
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if (!sock_fgfdm.bind("127.0.0.1", fdm_port)) {
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check_stdout();
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return false;
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}
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sock_fgfdm.set_blocking(false);
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sock_fgfdm.reuseaddress();
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opened_fdm_socket = true;
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return true;
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}
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/*
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decode and send servos
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*/
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void JSBSim::send_servos(const struct sitl_input &input)
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{
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char *buf = NULL;
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float aileron = (input.servos[0]-1500)/500.0f;
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float elevator = (input.servos[1]-1500)/500.0f;
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float throttle = (input.servos[2]-1000)/1000.0;
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float rudder = (input.servos[3]-1500)/500.0f;
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if (frame == FRAME_ELEVON) {
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// fake an elevon plane
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float ch1 = aileron;
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float ch2 = elevator;
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aileron = (ch2-ch1)/2.0f;
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// the minus does away with the need for RC2_REV=-1
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elevator = -(ch2+ch1)/2.0f;
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} else if (frame == FRAME_VTAIL) {
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// fake a vtail plane
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float ch1 = elevator;
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float ch2 = rudder;
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// this matches VTAIL_OUTPUT==2
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elevator = (ch2-ch1)/2.0f;
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rudder = (ch2+ch1)/2.0f;
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}
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2015-05-10 08:01:49 -03:00
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asprintf(&buf,
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"set fcs/aileron-cmd-norm %f\n"
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"set fcs/elevator-cmd-norm %f\n"
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"set fcs/rudder-cmd-norm %f\n"
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"set fcs/throttle-cmd-norm %f\n"
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2015-05-22 22:03:57 -03:00
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"set atmosphere/psiw-rad %f\n"
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"set atmosphere/wind-mag-fps %f\n"
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"step\n",
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aileron, elevator, rudder, throttle,
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radians(input.wind.direction),
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input.wind.speed / FEET_TO_METERS);
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2015-05-21 19:04:38 -03:00
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ssize_t buflen = strlen(buf);
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ssize_t sent = sock_control.send(buf, buflen);
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free(buf);
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if (sent < 0) {
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if (errno != EAGAIN) {
|
|
|
|
fprintf(stderr, "Fatal: Failed to send on control socket: %s\n",
|
|
|
|
strerror(errno));
|
|
|
|
exit(1);
|
|
|
|
}
|
|
|
|
}
|
|
|
|
if (sent < buflen) {
|
|
|
|
fprintf(stderr, "Failed to send all bytes on control socket\n");
|
|
|
|
}
|
2015-05-10 08:01:49 -03:00
|
|
|
}
|
|
|
|
|
2015-05-10 08:57:39 -03:00
|
|
|
/* nasty hack ....
|
|
|
|
JSBSim sends in little-endian
|
|
|
|
*/
|
|
|
|
void FGNetFDM::ByteSwap(void)
|
|
|
|
{
|
2015-05-10 08:01:49 -03:00
|
|
|
uint32_t *buf = (uint32_t *)this;
|
|
|
|
for (uint16_t i=0; i<sizeof(*this)/4; i++) {
|
|
|
|
buf[i] = ntohl(buf[i]);
|
|
|
|
}
|
2015-05-10 08:57:39 -03:00
|
|
|
// fixup the 3 doubles
|
2015-05-10 08:01:49 -03:00
|
|
|
buf = (uint32_t *)&longitude;
|
|
|
|
uint32_t tmp;
|
|
|
|
for (uint8_t i=0; i<3; i++) {
|
|
|
|
tmp = buf[0];
|
|
|
|
buf[0] = buf[1];
|
|
|
|
buf[1] = tmp;
|
|
|
|
buf += 2;
|
|
|
|
}
|
|
|
|
}
|
|
|
|
|
|
|
|
/*
|
|
|
|
receive an update from the FDM
|
|
|
|
This is a blocking function
|
|
|
|
*/
|
|
|
|
void JSBSim::recv_fdm(const struct sitl_input &input)
|
|
|
|
{
|
|
|
|
FGNetFDM fdm;
|
2015-05-10 08:57:39 -03:00
|
|
|
check_stdout();
|
2015-05-10 08:01:49 -03:00
|
|
|
while (sock_fgfdm.recv(&fdm, sizeof(fdm), 100) != sizeof(fdm)) {
|
|
|
|
send_servos(input);
|
|
|
|
check_stdout();
|
|
|
|
}
|
|
|
|
fdm.ByteSwap();
|
|
|
|
|
|
|
|
accel_body = Vector3f(fdm.A_X_pilot, fdm.A_Y_pilot, fdm.A_Z_pilot) * FEET_TO_METERS;
|
|
|
|
|
|
|
|
double p, q, r;
|
|
|
|
SITL::convert_body_frame(degrees(fdm.phi), degrees(fdm.theta),
|
|
|
|
degrees(fdm.phidot), degrees(fdm.thetadot), degrees(fdm.psidot),
|
|
|
|
&p, &q, &r);
|
|
|
|
gyro = Vector3f(p, q, r);
|
|
|
|
|
|
|
|
velocity_ef = Vector3f(fdm.v_north, fdm.v_east, fdm.v_down) * FEET_TO_METERS;
|
|
|
|
location.lat = degrees(fdm.latitude) * 1.0e7;
|
|
|
|
location.lng = degrees(fdm.longitude) * 1.0e7;
|
2015-05-10 08:57:39 -03:00
|
|
|
location.alt = fdm.agl*100 + home.alt;
|
2015-05-10 08:01:49 -03:00
|
|
|
dcm.from_euler(fdm.phi, fdm.theta, fdm.psi);
|
2015-05-22 22:24:10 -03:00
|
|
|
airspeed = fdm.vcas * FEET_TO_METERS;
|
2015-05-10 08:01:49 -03:00
|
|
|
|
|
|
|
// assume 1kHz for now
|
|
|
|
time_now_us += 1000;
|
|
|
|
}
|
|
|
|
|
2015-05-21 19:04:38 -03:00
|
|
|
void JSBSim::drain_control_socket()
|
|
|
|
{
|
|
|
|
const uint16_t buflen = 1024;
|
|
|
|
char buf[buflen];
|
|
|
|
ssize_t received;
|
|
|
|
do {
|
|
|
|
received = sock_control.recv(buf, buflen, 0);
|
|
|
|
if (received < 0) {
|
|
|
|
if (errno != EAGAIN && errno != EWOULDBLOCK) {
|
|
|
|
fprintf(stderr, "error recv on control socket: %s",
|
|
|
|
strerror(errno));
|
|
|
|
}
|
|
|
|
} else {
|
|
|
|
// fprintf(stderr, "received from control socket: %s\n", buf);
|
|
|
|
}
|
|
|
|
} while (received > 0);
|
|
|
|
}
|
2015-05-10 08:01:49 -03:00
|
|
|
/*
|
|
|
|
update the JSBSim simulation by one time step
|
|
|
|
*/
|
|
|
|
void JSBSim::update(const struct sitl_input &input)
|
|
|
|
{
|
|
|
|
while (!initialised) {
|
|
|
|
if (!create_templates() ||
|
|
|
|
!start_JSBSim() ||
|
|
|
|
!open_control_socket() ||
|
|
|
|
!open_fdm_socket()) {
|
|
|
|
time_now_us = 1;
|
|
|
|
return;
|
|
|
|
}
|
|
|
|
initialised = true;
|
|
|
|
}
|
|
|
|
send_servos(input);
|
|
|
|
recv_fdm(input);
|
|
|
|
adjust_frame_time(1000);
|
|
|
|
sync_frame_time();
|
2015-05-21 19:04:38 -03:00
|
|
|
drain_control_socket();
|
2015-05-10 08:01:49 -03:00
|
|
|
}
|
|
|
|
#endif // CONFIG_HAL_BOARD
|