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ardupilot/Tools/autotest/jsbsim/runsim.py

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#!/usr/bin/env python
# run a jsbsim model as a child process
import sys, os, pexpect, socket
import math, time, select, struct, signal, errno
sys.path.insert(0, os.path.join(os.path.dirname(os.path.realpath(__file__)), '..', 'pysim'))
import util, atexit, fdpexpect
from pymavlink import fgFDM
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_template(home):
'''setup aircraft/Rascal/reset.xml'''
global opts
v = home.split(',')
if len(v) != 4:
print("home should be lat,lng,alt,hdg - '%s'" % home)
sys.exit(1)
latitude = float(v[0])
longitude = float(v[1])
altitude = float(v[2])
heading = float(v[3])
sitl_state.ground_height = altitude
template = os.path.join('aircraft', 'Rascal', 'reset_template.xml')
reset = os.path.join('aircraft', 'Rascal', 'reset.xml')
xml = open(template).read() % { 'LATITUDE' : str(latitude),
'LONGITUDE' : str(longitude),
'HEADING' : str(heading) }
open(reset, mode='w').write(xml)
print("Wrote %s" % reset)
baseport = int(opts.simout.split(':')[1])
template = os.path.join('jsbsim', 'fgout_template.xml')
out = os.path.join('jsbsim', 'fgout.xml')
xml = open(template).read() % { 'FGOUTPORT' : str(baseport+3) }
open(out, mode='w').write(xml)
print("Wrote %s" % out)
template = os.path.join('jsbsim', 'rascal_test_template.xml')
out = os.path.join('jsbsim', 'rascal_test.xml')
xml = open(template).read() % { 'JSBCONSOLEPORT' : str(baseport+4) }
open(out, mode='w').write(xml)
print("Wrote %s" % out)
def process_sitl_input(buf):
'''process control changes from SITL sim'''
control = list(struct.unpack('<14H', buf))
pwm = control[:11]
(speed, direction, turbulance) = control[11:]
global wind
wind.speed = speed*0.01
wind.direction = direction*0.01
wind.turbulance = turbulance*0.01
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 opts.elevon:
# fake an elevon plane
ch1 = aileron
ch2 = elevator
aileron = (ch2-ch1)/2.0
# the minus does away with the need for RC2_REV=-1
elevator = -(ch2+ch1)/2.0
if opts.vtail:
# fake an elevon plane
ch1 = elevator
ch2 = rudder
# this matches VTAIL_OUTPUT==2
elevator = (ch2-ch1)/2.0
rudder = (ch2+ch1)/2.0
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('<17dI',
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('v_down', 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'),
0x4c56414f)
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("--elevon", action='store_true', default=False, help='assume elevon input')
parser.add_option("--vtail", action='store_true', default=False, help='assume vtail input')
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)
setup_template(opts.home)
# 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)
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(28)
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')
# only simulate wind above 5 meters, to prevent crashes while
# waiting for takeoff
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
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