#!/usr/bin/env python # run a jsbsim model as a child process import sys, os, pexpect, fdpexpect, socket import math, time, select, struct, signal, errno sys.path.insert(0, os.path.join(os.path.dirname(os.path.realpath(__file__)), '..', 'pysim')) sys.path.insert(0, os.path.join(os.path.dirname(os.path.realpath(__file__)), '..', 'pymavlink')) import util, fgFDM, atexit class control_state(object): def __init__(self): self.aileron = 0 self.elevator = 0 self.throttle = 0 self.rudder = 0 self.ground_height = 0 sitl_state = control_state() def interpret_address(addrstr): '''interpret a IP:port string''' a = addrstr.split(':') a[1] = int(a[1]) return tuple(a) def jsb_set(variable, value): '''set a JSBSim variable''' global jsb_console jsb_console.send('set %s %s\r\n' % (variable, value)) def setup_home(home): '''setup home location''' v = home.split(',') if len(v) != 4: print("home should be lat,lng,alt,hdg") sys.exit(1) latitude = float(v[0]) longitude = float(v[1]) altitude = float(v[2]) heading = float(v[3]) sitl_state.ground_height = altitude jsb_set('position/lat-gc-deg', latitude) jsb_set('position/long-gc-deg', longitude) jsb_set('attitude/psi-rad', math.radians(heading)) jsb_set('attitude/phi-rad', 0) jsb_set('attitude/theta-rad', 0) def process_sitl_input(buf): '''process control changes from SITL sim''' pwm = list(struct.unpack('<11H', buf)) aileron = (pwm[0]-1500)/500.0 elevator = (pwm[1]-1500)/500.0 throttle = (pwm[2]-1000)/1000.0 rudder = (pwm[3]-1500)/500.0 if aileron != sitl_state.aileron: jsb_set('fcs/aileron-cmd-norm', aileron) sitl_state.aileron = aileron if elevator != sitl_state.elevator: jsb_set('fcs/elevator-cmd-norm', elevator) sitl_state.elevator = elevator if rudder != sitl_state.rudder: jsb_set('fcs/rudder-cmd-norm', rudder) sitl_state.rudder = rudder if throttle != sitl_state.throttle: jsb_set('fcs/throttle-cmd-norm', throttle) sitl_state.throttle = throttle def update_wind(wind): '''update wind simulation''' (speed, direction) = wind.current() jsb_set('atmosphere/psiw-rad', math.radians(direction)) jsb_set('atmosphere/wind-mag-fps', speed/0.3048) def process_jsb_input(buf): '''process FG FDM input from JSBSim''' global fdm, fg_out, sim_out fdm.parse(buf) if fg_out: try: agl = fdm.get('agl', units='meters') fdm.set('altitude', agl+sitl_state.ground_height, units='meters') fdm.set('rpm', sitl_state.throttle*1000) fg_out.send(fdm.pack()) except socket.error as e: if e.errno not in [ errno.ECONNREFUSED ]: raise simbuf = struct.pack('<16dI', fdm.get('latitude', units='degrees'), fdm.get('longitude', units='degrees'), fdm.get('altitude', units='meters'), fdm.get('psi', units='degrees'), fdm.get('v_north', units='mps'), fdm.get('v_east', units='mps'), fdm.get('A_X_pilot', units='mpss'), fdm.get('A_Y_pilot', units='mpss'), fdm.get('A_Z_pilot', units='mpss'), fdm.get('phidot', units='dps'), fdm.get('thetadot', units='dps'), fdm.get('psidot', units='dps'), fdm.get('phi', units='degrees'), fdm.get('theta', units='degrees'), fdm.get('psi', units='degrees'), fdm.get('vcas', units='mps'), 0x4c56414e) try: sim_out.send(simbuf) except socket.error as e: if e.errno not in [ errno.ECONNREFUSED ]: raise ################## # main program from optparse import OptionParser parser = OptionParser("runsim.py [options]") parser.add_option("--simin", help="SITL input (IP:port)", default="127.0.0.1:5502") parser.add_option("--simout", help="SITL output (IP:port)", default="127.0.0.1:5501") parser.add_option("--fgout", help="FG display output (IP:port)", default="127.0.0.1:5503") parser.add_option("--home", type='string', help="home lat,lng,alt,hdg (required)") parser.add_option("--script", type='string', help='jsbsim model script', default='jsbsim/rascal_test.xml') parser.add_option("--options", type='string', help='jsbsim startup options') parser.add_option("--wind", dest="wind", help="Simulate wind (speed,direction,turbulance)", default='0,0,0') (opts, args) = parser.parse_args() for m in [ 'home', 'script' ]: if not opts.__dict__[m]: print("Missing required option '%s'" % m) parser.print_help() sys.exit(1) os.chdir(util.reltopdir('Tools/autotest')) # kill off child when we exit atexit.register(util.pexpect_close_all) # start child cmd = "JSBSim --realtime --suspend --nice --simulation-rate=1000 --logdirectivefile=jsbsim/fgout.xml --script=%s" % opts.script if opts.options: cmd += ' %s' % opts.options jsb = pexpect.spawn(cmd, logfile=sys.stdout, timeout=10) jsb.delaybeforesend = 0 util.pexpect_autoclose(jsb) i = jsb.expect(["Successfully bound to socket for input on port (\d+)", "Could not bind to socket for input"]) if i == 1: print("Failed to start JSBSim - is another copy running?") sys.exit(1) jsb_out_address = interpret_address("127.0.0.1:%u" % int(jsb.match.group(1))) jsb.expect("Creating UDP socket on port (\d+)") jsb_in_address = interpret_address("127.0.0.1:%u" % int(jsb.match.group(1))) jsb.expect("Successfully connected to socket for output") jsb.expect("JSBSim Execution beginning") # setup output to jsbsim print("JSBSim console on %s" % str(jsb_out_address)) jsb_out = socket.socket(socket.AF_INET, socket.SOCK_STREAM) jsb_out.connect(jsb_out_address) jsb_console = fdpexpect.fdspawn(jsb_out.fileno(), logfile=sys.stdout) jsb_console.delaybeforesend = 0 # setup input from jsbsim print("JSBSim FG FDM input on %s" % str(jsb_in_address)) jsb_in = socket.socket(socket.AF_INET, socket.SOCK_DGRAM) jsb_in.bind(jsb_in_address) jsb_in.setblocking(0) # socket addresses sim_out_address = interpret_address(opts.simout) sim_in_address = interpret_address(opts.simin) # setup input from SITL sim sim_in = socket.socket(socket.AF_INET, socket.SOCK_DGRAM) sim_in.bind(sim_in_address) sim_in.setblocking(0) # setup output to SITL sim sim_out = socket.socket(socket.AF_INET, socket.SOCK_DGRAM) sim_out.connect(interpret_address(opts.simout)) sim_out.setblocking(0) # setup possible output to FlightGear for display fg_out = None if opts.fgout: fg_out = socket.socket(socket.AF_INET, socket.SOCK_DGRAM) fg_out.connect(interpret_address(opts.fgout)) # setup wind generator wind = util.Wind(opts.wind) setup_home(opts.home) fdm = fgFDM.fgFDM() jsb_console.send('info\n') jsb_console.send('resume\n') jsb.expect("trim computation time") time.sleep(1.5) jsb_console.logfile = None print("Simulator ready to fly") def main_loop(): '''run main loop''' tnow = time.time() last_report = tnow last_sim_input = tnow last_wind_update = tnow frame_count = 0 paused = False while True: rin = [jsb_in.fileno(), sim_in.fileno(), jsb_console.fileno(), jsb.fileno()] try: (rin, win, xin) = select.select(rin, [], [], 1.0) except select.error: util.check_parent() continue tnow = time.time() if jsb_in.fileno() in rin: buf = jsb_in.recv(fdm.packet_size()) process_jsb_input(buf) frame_count += 1 if sim_in.fileno() in rin: simbuf = sim_in.recv(22) process_sitl_input(simbuf) last_sim_input = tnow # show any jsbsim console output if jsb_console.fileno() in rin: util.pexpect_drain(jsb_console) if jsb.fileno() in rin: util.pexpect_drain(jsb) if tnow - last_sim_input > 0.2: if not paused: print("PAUSING SIMULATION") paused = True jsb_console.send('hold\n') else: if paused: print("RESUMING SIMULATION") paused = False jsb_console.send('resume\n') if tnow - last_wind_update > 0.1: update_wind(wind) last_wind_update = tnow if tnow - last_report > 3: print("FPS %u asl=%.1f agl=%.1f roll=%.1f pitch=%.1f a=(%.2f %.2f %.2f)" % ( frame_count / (time.time() - last_report), fdm.get('altitude', units='meters'), fdm.get('agl', units='meters'), fdm.get('phi', units='degrees'), fdm.get('theta', units='degrees'), fdm.get('A_X_pilot', units='mpss'), fdm.get('A_Y_pilot', units='mpss'), fdm.get('A_Z_pilot', units='mpss'))) frame_count = 0 last_report = time.time() def exit_handler(): '''exit the sim''' signal.signal(signal.SIGINT, signal.SIG_IGN) signal.signal(signal.SIGTERM, signal.SIG_IGN) # JSBSim really doesn't like to die ... if getattr(jsb, 'pid', None) is not None: os.kill(jsb.pid, signal.SIGKILL) jsb_console.send('quit\n') jsb.close(force=True) util.pexpect_close_all() sys.exit(1) signal.signal(signal.SIGINT, exit_handler) signal.signal(signal.SIGTERM, exit_handler) try: main_loop() except: exit_handler() raise