def test_send_event(self):
sm = create_autospec(SimConnect.SimConnect)
pl1 = SimConnect.Plane(sm=sm)
pl1.send(SimConnect.Event.GEAR_DOWN)
pl1.gear_up
pl2 = SimConnect.Plane(sm=sm, add_default=False)
with self.assertRaises(AttributeError):
pl2.gear_up
def calcTodDegrees():
try:
sm = SimConnect()
aq = AircraftRequests(sm)
finalAlt = float(finalAltEntry.get())
alt = aq.get("PLANE_ALTITUDE")
y = finalAlt - alt
x = (y / math.tan(math.radians(-2.6))) / 6076.12
sm.exit()
todLabel.config(text="Descent Distance " + str(math.floor(x)))
except Exception:
todLabel.config(text="Could not connect to simulator!")
def calcTodVert():
try:
sm = SimConnect()
aq = AircraftRequests(sm)
vertSpeed = float(vertSpeedEntry.get())
groundSpeed = aq.get("GROUND_VELOCITY")
alt = aq.get("PLANE_ALTITUDE")
finalAlt = float(finalAltEntry.get())
y = alt - finalAlt
distance = ((y / vertSpeed) / 60) * groundSpeed
todLabel.config(text="Descent Distance: " +
str(math.floor(distance)))
sm.exit()
except Exception:
todLabel.config(text="Could not connect to simulator!")
def test_values(self):
sm = create_autospec(SimConnect.SimConnect)
def side_effect(*args, **kwargs):
def val():
v = 100
x = 100
while True:
yield x
x += v
data = sData()
val = val()
data["Altitude"] = next(val)
data["Latitude"] = next(val)
data["Longitude"] = next(val)
data["Kohlsman"] = next(val)
return data
sm.get_data.side_effect = side_effect
pl = SimConnect.Plane(sm=sm)
self.assertEqual(100, pl.altitude)
self.assertEqual(200, pl.latitude)
self.assertEqual(300, pl.longitude)
self.assertEqual(400, pl.kohlsman)
def simconnect_thread_func2(threadname):
global ui_friendly_dictionary
while True:
try:
sm = SimConnect()
break
except:
None
ae = AircraftEvents(sm)
aq = AircraftRequests(sm)
def thousandify(x):
return f"{x:,}"
async def ui_dictionary(ui_friendly_dictionary):
# Additional for performance
ui_friendly_dictionary["LATITUDE"] = round(await aq.get("PLANE_LATITUDE"), 6)
ui_friendly_dictionary["LONGITUDE"] = round(await aq.get("PLANE_LONGITUDE"), 6)
ui_friendly_dictionary["AUTOPILOT_HEADING_LOCK_DIR"] = round(await aq.get("AUTOPILOT_HEADING_LOCK_DIR"))
ui_friendly_dictionary["AUTOPILOT_ALTITUDE_LOCK_VAR"] = thousandify(round(await aq.get("AUTOPILOT_ALTITUDE_LOCK_VAR")))
ui_friendly_dictionary["AUTOPILOT_VERTICAL_HOLD_VAR"] = await aq.get("AUTOPILOT_VERTICAL_HOLD_VAR")
ui_friendly_dictionary["AUTOPILOT_AIRSPEED_HOLD_VAR"] = round(await aq.get("AUTOPILOT_AIRSPEED_HOLD_VAR"))
# NAV/ADF Compass Settings
ui_friendly_dictionary["NAV1_OBS_DEG"] = round(await aq.get("NAV_OBS:1"), 0)
ui_friendly_dictionary["ADF_CARD_DEG"] = round(await aq.get("ADF_CARD"), 0)
ui_friendly_dictionary["NAV2_OBS_DEG"] = round(await aq.get("NAV_OBS:2"), 0)
while True:
asyncio.run(ui_dictionary(ui_friendly_dictionary))
def cruise(self):
points = 20
random.seed(0)
cg = 0.33
error_alt = 1
error_ias = 1
actual_vs = 1000
# Read the Aircraft Data file
df = data.data_read('CRZ')
logger.test_header(self, "CRZ")
start_time = time.time()
i = 1
# Random Aircraft situation
weight, altitude, ias = data.a32x_state(df)
logger.test_env(self, weight, altitude, ias, i, points)
# Create the SimConnect link
sm = SimConnect()
aq = AircraftRequests(sm, _time=0)
ae = AircraftEvents(sm)
# Check and set initial aircraft settings:
# AP1 ON, ATHR ON, FD ON & CLB
ac_init(aq, ae)
# Set Weight and CG ... this goes first to avoid excessive dumping
W_n_B(aq, weight, cg)
# Main test point routine - Setting stable aircraft conditions
crz_alt_ias(sm, aq, ae, altitude, ias)
# Altitude & Speed damping "filter". Use VS first as a measure
# of stability
# To avoid excesive damping, fuel and CG are set first with
# enough headroom
while error_alt > 1 or error_ias > 1 or abs(actual_vs) > 10:
actual_alt = aq.get("INDICATED_ALTITUDE")
actual_ias = aq.get("AIRSPEED_INDICATED")
actual_vs = aq.get("VERTICAL_SPEED")
error_alt = round(abs((actual_alt - altitude) / altitude) * 100, 3)
error_ias = round(abs((actual_ias - ias) / ias) * 100, 3)
elapsed_time = time.time() - start_time
msg = "Tolerance Figures - Alt: " + str(
error_alt) + "% IAS: " + str(error_ias) + "% VS: " + str(
round(actual_vs,
1)) + "fpm Elapsed Time - " + str(
round(elapsed_time, 2)) + " secs."
self.updateStatus(msg)
QtCore.QCoreApplication.processEvents()
#print(error_alt, " ", error_ias, " ", actual_vs)
print(aq.get("TOTAL_WEIGHT"))
print(aq.get("CG_PERCENT"))
def lbsClick():
try:
lbs = float(lbsEntry.get())
sm = SimConnect()
ae = AircraftEvents(sm)
ar = AircraftRequests(sm)
setFuel = ae.find("ADD_FUEL_QUANTITY")
totalQuantity = ar.get("FUEL_TOTAL_QUANTITY")
totalCapacitygal = ar.get("FUEL_TOTAL_CAPACITY")
weightPerGallon = ar.get("FUEL_WEIGHT_PER_GALLON")
totalCapacity = totalCapacitygal * weightPerGallon
fuelToAdd = (lbs / totalCapacity) * 65535
print(totalCapacity)
print(totalQuantity)
print(fuelToAdd)
setFuel(int(fuelToAdd))
sm.exit()
fuelLabel.config(text="Fuel Loaded!")
except Exception:
fuelLabel.config(text="Could not connect to sim!")
def connect():
global sm
global ae
global aq
if sm == None:
try:
sm = SimConnect()
ae = AircraftEvents(sm)
aq = AircraftRequests(sm, _time=10)
return 'success'
except:
return 'Failed to connect to the Simulator', 500
return 'success'
def main():
# Initialize program state
DONE = False
# Initialize pygame
pygame.init()
screen = pygame.display.set_mode((200, 50)) # Need this to pick up events
clock = pygame.time.Clock()
# Initialize joysticks
joysticks = []
pygame.joystick.init()
joystick_count = pygame.joystick.get_count()
print("Found devices:")
for i in range(joystick_count):
joysticks.append(pygame.joystick.Joystick(i))
joysticks[i].init()
print("{name} - ID: {id}".format(
name=joysticks[i].get_name(),
id=joysticks[i].get_id(),
))
# Initialize SimConnect and adapters
sim_connect = SimConnect()
vor_adapter = VorAdapter(sim_connect)
# Check for events
while not DONE:
for event in pygame.event.get():
if event.type == pygame.QUIT:
DONE = True
vor_adapter.handle_event(event)
clock.tick(20)
# Quit
sim_connect.exit()
pygame.quit()
def calcTodDist():
try:
sm = SimConnect()
aq = AircraftRequests(sm)
alt = aq.get("PLANE_ALTITUDE")
groundSpeed = aq.get("GROUND_VELOCITY")
finalAlt = float(finalAltEntry.get())
dist = float(distanceEntry.get())
y = alt - finalAlt
vertSpeed = (y * groundSpeed) / (dist * 60)
todLabel.config(text="Vertical Speed: " +
str(math.floor(vertSpeed)))
except Exception:
todLabel.config(text="Could not connect to simulator!")
def get_it(self, *args, **kwargs):
try:
sm = SimConnect()
except ConnectionError:
self.SetStatusText("Pretty sure flight sim is closed")
return
if not sm:
self.SetStatusText("Pretty sure flight sim is closed")
return
aq = AircraftRequests(sm, _time=500)
latlng = (aq.get("PLANE_LATITUDE"), aq.get("PLANE_LONGITUDE"))
if int(latlng[0] * 10) == 0 and int(latlng[0] * 10) == 0:
self.SetStatusText("Pretty sure you're not flying right now")
return
webbrowser.open(f'https://www.google.com/maps/?q={latlng}')
self.SetStatusText(latlng)
def init_simconnect(defaultRefreshTime: int):
global aq
global sm
try:
sm = SimConnect()
except:
print("Unexpected error, ", sys.exc_info()[0])
return
if sm:
print("Succesful SimConnect call: ", sm)
else:
print("Unsuccesful Simconnect call, exiting.")
return
aq = AircraftRequests(sm, _time=defaultRefreshTime)
def initAll(defaultRefreshTime: int):
global aq
global sm
try:
sm = SimConnect()
except:
print("Unexpected error, ", sys.exc_info()[0])
return
if sm:
print("Succesful SimConnect call: ", sm)
else:
print("Unsuccesful Simconnect call, exiting.")
return
# Note the default _time is 2000 to be refreshed every 2 seconds
aq = AircraftRequests(sm, _time=defaultRefreshTime)
def simconnect_thread_func(threadname):
global ui_friendly_dictionary
global event_name
global value_to_use
global sm
global ae
while True:
try:
sm = SimConnect()
print("\n********* MSFS 2020 Mobile Companion App *********\n")
print(f"Local web server for MSFS 2020 Mobile Companion App initialized.\n")
print(f"Launch {socket.gethostbyname(socket.gethostname())}:4000 in your browser to access MSFS 2020 Mobile Companion App.\n")
print(f"Make sure your your mobile device is connected to the same local network (WIFI) as this PC.\n")
print(f"Notice: If your computer has more than one active ethernet/WIFI adapter, please check ipconfig in command prompt.\n")
print("**************************************************\n\n")
break
except:
print("Could not find MSFS running. Please launch MSFS first and then restart the MSFS 2020 Mobile Companion App.")
sleep(5)
ae = AircraftEvents(sm)
aq = AircraftRequests(sm)
# Initialize previous altitude for code stability
previous_alt = -400
# Initialize vars for landing info
ui_friendly_dictionary["LANDING_VS1"] = "N/A"
ui_friendly_dictionary["LANDING_T1"] = 0
ui_friendly_dictionary["LANDING_VS2"] = "N/A"
ui_friendly_dictionary["LANDING_T2"] = 0
ui_friendly_dictionary["LANDING_VS3"] = "N/A"
ui_friendly_dictionary["LANDING_T3"] = 0
def thousandify(x):
return f"{x:,}"
async def ui_dictionary(ui_friendly_dictionary, previous_alt, landing_t1, landing_vs1, landing_t2, landing_vs2, landing_t3, landing_vs3):
# Position
try:
ui_friendly_dictionary["LATITUDE"] = round(await aq.get("PLANE_LATITUDE"),6)
ui_friendly_dictionary["LONGITUDE"] = round(await aq.get("PLANE_LONGITUDE"),6)
ui_friendly_dictionary["MAGNETIC_COMPASS"] = round(round(await aq.get("PLANE_HEADING_DEGREES_TRUE"),2) * 180/3.1416, 2)
#ui_friendly_dictionary["MAGVAR"] = round(await aq.get("MAGVAR"))
except:
None
# Radios
ui_friendly_dictionary["NAV1_STANDBY"] = round(await aq.get("NAV_STANDBY_FREQUENCY:1"),2)
ui_friendly_dictionary["NAV1_ACTIVE"] = round(await aq.get("NAV_ACTIVE_FREQUENCY:1"),2)
ui_friendly_dictionary["NAV2_STANDBY"] = round(await aq.get("NAV_STANDBY_FREQUENCY:2"),2)
ui_friendly_dictionary["NAV2_ACTIVE"] = round(await aq.get("NAV_ACTIVE_FREQUENCY:2"),2)
# ADF Active
adf_use_bcd = int(await aq.get("ADF_ACTIVE_FREQUENCY:1"))
adf_use_digits = ""
for i in reversed(range(4)):
adf_use_digit = math.floor(adf_use_bcd / (65536*(16**i)))
adf_use_digits = adf_use_digits + str(adf_use_digit)
adf_use_bcd = adf_use_bcd - (65536*(16**i)) * adf_use_digit
try:
ui_friendly_dictionary["ADF_USE_1000"] = adf_use_digits[0]
ui_friendly_dictionary["ADF_USE_100"] = adf_use_digits[1]
ui_friendly_dictionary["ADF_USE_10"] = adf_use_digits[2]
ui_friendly_dictionary["ADF_USE_1"] = adf_use_digits[3]
ui_friendly_dictionary["ADF_USE"] = int(adf_use_digits)
except:
None
# ADF Standby
adf_stby = int(await aq.get("ADF_STANDBY_FREQUENCY:1"))/1000
try:
if adf_stby >= 1000:
ui_friendly_dictionary["ADF_STBY_1000"] = str(adf_stby)[0]
ui_friendly_dictionary["ADF_STBY_100"] = str(adf_stby)[1]
ui_friendly_dictionary["ADF_STBY_10"] = str(adf_stby)[2]
ui_friendly_dictionary["ADF_STBY_1"] = str(adf_stby)[3]
else:
ui_friendly_dictionary["ADF_STBY_1000"] = "0"
ui_friendly_dictionary["ADF_STBY_100"] = str(adf_stby)[0]
ui_friendly_dictionary["ADF_STBY_10"] = str(adf_stby)[1]
ui_friendly_dictionary["ADF_STBY_1"] = str(adf_stby)[2]
except:
None
# NAV/ADF Compass Settings
ui_friendly_dictionary["NAV1_OBS_DEG"] = round(await aq.get("NAV_OBS:1"),0)
ui_friendly_dictionary["ADF_CARD_DEG"] = round(await aq.get("ADF_CARD"),0)
ui_friendly_dictionary["NAV2_OBS_DEG"] = round(await aq.get("NAV_OBS:2"),0)
# Comms
ui_friendly_dictionary["COM1_STANDBY"] = round(await aq.get("COM_STANDBY_FREQUENCY:1"),3)
ui_friendly_dictionary["COM1_ACTIVE"] = round(await aq.get("COM_ACTIVE_FREQUENCY:1"),3)
ui_friendly_dictionary["COM1_TRANSMIT"] = await aq.get("COM_TRANSMIT:1")
ui_friendly_dictionary["COM2_STANDBY"] = round(await aq.get("COM_STANDBY_FREQUENCY:2"),3)
ui_friendly_dictionary["COM2_ACTIVE"] = round(await aq.get("COM_ACTIVE_FREQUENCY:2"),3)
ui_friendly_dictionary["COM2_TRANSMIT"] = await aq.get("COM_TRANSMIT:2")
# XPNDR
xpndr_bcd = await aq.get("TRANSPONDER_CODE:1")
xpndr_digits = ""
# XPNDR Conversion from BCD to Decimal
try:
for i in reversed(range(4)):
xpndr_digit = math.floor(xpndr_bcd / (16**i))
xpndr_digits = xpndr_digits + str(xpndr_digit)
xpndr_bcd = xpndr_bcd - (16**i) * xpndr_digit
except:
None
try:
ui_friendly_dictionary["XPNDR_1000"] = xpndr_digits[0]
ui_friendly_dictionary["XPNDR_100"] = xpndr_digits[1]
ui_friendly_dictionary["XPNDR_10"] = xpndr_digits[2]
ui_friendly_dictionary["XPNDR_1"] = xpndr_digits[3]
ui_friendly_dictionary["XPNDR"] = int(xpndr_digits)
except:
None
# Autopilot
ui_friendly_dictionary["AUTOPILOT_MASTER"] = await aq.get("AUTOPILOT_MASTER")
ui_friendly_dictionary["AUTOPILOT_NAV1_LOCK"] = await aq.get("AUTOPILOT_NAV1_LOCK")
ui_friendly_dictionary["AUTOPILOT_HEADING_LOCK"] = await aq.get("AUTOPILOT_HEADING_LOCK")
ui_friendly_dictionary["AUTOPILOT_HEADING_LOCK_DIR"] = round(await aq.get("AUTOPILOT_HEADING_LOCK_DIR"))
ui_friendly_dictionary["AUTOPILOT_ALTITUDE_LOCK"] = await aq.get("AUTOPILOT_ALTITUDE_LOCK")
ui_friendly_dictionary["AUTOPILOT_ALTITUDE_LOCK_VAR"] = thousandify(round(await aq.get("AUTOPILOT_ALTITUDE_LOCK_VAR")))
ui_friendly_dictionary["AUTOPILOT_GLIDESLOPE_HOLD"] = await aq.get("AUTOPILOT_GLIDESLOPE_HOLD")
ui_friendly_dictionary["AUTOPILOT_APPROACH_HOLD"] = await aq.get("AUTOPILOT_APPROACH_HOLD")
ui_friendly_dictionary["AUTOPILOT_BACKCOURSE_HOLD"] = await aq.get("AUTOPILOT_BACKCOURSE_HOLD")
ui_friendly_dictionary["AUTOPILOT_VERTICAL_HOLD"] = await aq.get("AUTOPILOT_VERTICAL_HOLD")
ui_friendly_dictionary["AUTOPILOT_VERTICAL_HOLD_VAR"] = await aq.get("AUTOPILOT_VERTICAL_HOLD_VAR")
ui_friendly_dictionary["AUTOPILOT_FLIGHT_LEVEL_CHANGE"] = await aq.get("AUTOPILOT_FLIGHT_LEVEL_CHANGE")
ui_friendly_dictionary["AUTOPILOT_AIRSPEED_HOLD_VAR"] = round(await aq.get("AUTOPILOT_AIRSPEED_HOLD_VAR"))
ui_friendly_dictionary["AUTOPILOT_AUTOTHROTTLE"] = await aq.get("AUTOTHROTTLE_ACTIVE")
ui_friendly_dictionary["AIRSPEED_INDICATED"] = round(await aq.get("AIRSPEED_INDICATED"))
# Placeholders - Not Actively Used for stress testing
#ui_friendly_dictionary["AUTOPILOT_NAV_SELECTED"] = await aq.get("AUTOPILOT_NAV_SELECTED")
#ui_friendly_dictionary["AUTOPILOT_WING_LEVELER"] = await aq.get("AUTOPILOT_WING_LEVELER")
#ui_friendly_dictionary["AUTOPILOT_PITCH_HOLD"] = await aq.get("AUTOPILOT_PITCH_HOLD")
#ui_friendly_dictionary["AUTOPILOT_PITCH_HOLD_REF"] = await aq.get("AUTOPILOT_PITCH_HOLD_REF")
ui_friendly_dictionary["AUTOPILOT_FLIGHT_DIRECTOR_ACTIVE"] = await aq.get("AUTOPILOT_FLIGHT_DIRECTOR_ACTIVE")
# Lights
ui_friendly_dictionary["LIGHT_LANDING"] = await aq.get("LIGHT_LANDING")
ui_friendly_dictionary["LIGHT_TAXI"] = await aq.get("LIGHT_TAXI")
ui_friendly_dictionary["LIGHT_STROBE"] = await aq.get("LIGHT_STROBE")
ui_friendly_dictionary["LIGHT_NAV"] = await aq.get("LIGHT_NAV")
ui_friendly_dictionary["LIGHT_BEACON"] = await aq.get("LIGHT_BEACON")
ui_friendly_dictionary["LIGHT_CABIN"] = await aq.get("LIGHT_CABIN")
ui_friendly_dictionary["LIGHT_LOGO"] = await aq.get("LIGHT_CABIN")
ui_friendly_dictionary["LIGHT_PANEL"] = await aq.get("LIGHT_PANEL")
ui_friendly_dictionary["LIGHT_WING"] = await aq.get("LIGHT_WING")
ui_friendly_dictionary["LIGHT_RECOGNITION"] = await aq.get("LIGHT_RECOGNITION")
# Pitot Heat and Deice
ui_friendly_dictionary["PITOT_HEAT"] = await aq.get("PITOT_HEAT")
#ui_friendly_dictionary["PROP_DEICE_SWITCH"] = await aq.get("PROP_DEICE_SWITCH:1")
ui_friendly_dictionary["ENG_ANTI_ICE"] = await aq.get("ENG_ANTI_ICE:1")
#ui_friendly_dictionary["GEN_ENG_ANTI_ICE"] = await aq.get("GENERAL_ENG_ANTI_ICE_POSITION:1")
ui_friendly_dictionary["STRUCTURAL_DEICE_SWITCH"] = await aq.get("STRUCTURAL_DEICE_SWITCH")
#ui_friendly_dictionary["PANEL_ANTI_ICE_SWITCH"] = await aq.get("PANEL_ANTI_ICE_SWITCH")
# Sim Rate
ui_friendly_dictionary["SIMULATION_RATE"] = await aq.get("SIMULATION_RATE")
# GPS Next Waypoint
ui_friendly_dictionary["NEXT_WP_LAT"] = await aq.get("GPS_WP_NEXT_LAT")
ui_friendly_dictionary["NEXT_WP_LON"] = await aq.get("GPS_WP_NEXT_LON")
# Current altitude
current_alt = await aq.get("INDICATED_ALTITUDE")
if current_alt > -300:
ui_friendly_dictionary["INDICATED_ALTITUDE"] = round(current_alt)
previous_alt = current_alt
else:
try:
ui_friendly_dictionary["INDICATED_ALTITUDE"] = previous_alt
except:
pass
# LOC and APPR Mode
try:
if (ui_friendly_dictionary["AUTOPILOT_APPROACH_HOLD"] == 1 and ui_friendly_dictionary["AUTOPILOT_GLIDESLOPE_HOLD"] == 1):
ui_friendly_dictionary["AUTOPILOT_APPR_MODE"] = 1
else:
ui_friendly_dictionary["AUTOPILOT_APPR_MODE"] = 0
if (ui_friendly_dictionary["AUTOPILOT_APPROACH_HOLD"] == 1 and ui_friendly_dictionary["AUTOPILOT_GLIDESLOPE_HOLD"] == 0):
ui_friendly_dictionary["AUTOPILOT_LOC_MODE"] = 1
else:
ui_friendly_dictionary["AUTOPILOT_LOC_MODE"] = 0
except:
None
# Other
current_landing = round(await aq.get("PLANE_TOUCHDOWN_NORMAL_VELOCITY") * 60)
current_time = datetime.datetime.now().strftime('%H:%M:%S')
if landing_vs1 != current_landing:
# Move 2nd to 3rd
landing_t3 = landing_t2
landing_vs3 = landing_vs2
# Move 1st to 2nd
landing_t2 = landing_t1
landing_vs2 = landing_vs1
# Assign new 1st
landing_t1 = current_time
landing_vs1 = current_landing
# Dictionary Output
ui_friendly_dictionary["LANDING_VS1"] = landing_vs1
ui_friendly_dictionary["LANDING_T1"] = landing_t1
ui_friendly_dictionary["LANDING_VS2"] = landing_vs2
ui_friendly_dictionary["LANDING_T2"] = landing_t2
ui_friendly_dictionary["LANDING_VS3"] = landing_vs3
ui_friendly_dictionary["LANDING_T3"] = landing_t3
while True:
asyncio.run(ui_dictionary(ui_friendly_dictionary, previous_alt, ui_friendly_dictionary["LANDING_T1"], ui_friendly_dictionary["LANDING_VS1"], ui_friendly_dictionary["LANDING_T2"], ui_friendly_dictionary["LANDING_VS2"], ui_friendly_dictionary["LANDING_T3"], ui_friendly_dictionary["LANDING_VS3"]))
from SimConnect import *
import logging
from SimConnect.Enum import *
from time import sleep
logging.basicConfig(level=logging.DEBUG)
LOGGER = logging.getLogger(__name__)
LOGGER.info("START")
# time holder for inline commands
ct_g = millis()
# creat simconnection and pass used user classes
sm = SimConnect()
aq = AircraftRequests(sm)
ae = AircraftEvents(sm)
mc = aq.find("MAGNETIC_COMPASS")
mv = aq.find("MAGVAR")
print(mc.get() + mv.get())
sm.exit()
quit()
# Set pos arund space nedle in WA.
sm.set_pos(
_Altitude=1000.0,
_Latitude=47.614699,
_Longitude=-122.358473,
_Airspeed=130,
_Heading=70.0,
# _Pitch=0.0,
debug = "OFF"
engine = tts.init()
def sayit(text):
engine.say(text)
engine.runAndWait()
simconnect_path = os.getcwd() + "/SimConnect.dll"
if debug == "OFF":
# Create SimConnect link
while True:
try:
sm = SimConnect(library_path=simconnect_path)
break
except:
print("Could not find MSFS running. Please launch MSFS.")
sleep(5)
# Note the default _time is 2000 to be refreshed every 2 seconds
aq = AircraftRequests(sm, _time=1000)
# Use _time=ms where ms is the time in milliseconds to cache the data.
# Setting ms to 0 will disable data caching and always pull new data from the sim.
# There is still a timeout of 4 tries with a 10ms delay between checks.
# If no data is received in 40ms the value will be set to None
# Each request can be fine tuned by setting the time param.
# To find and set timeout of cached data to 200ms:
#altitude = aq.find("PLANE_ALTITUDE")
def cruise(self):
rnd = 1
points = 200
random.seed(0)
cg = 0.27
error_alt = 1
error_tas = 1
actual_vs = 1000
n = 1
# Read the Aircraft Data file
df = data.data_read('CRZ')
logger.test_header(self, "CRZ")
if os.path.exists("test.txt"):
os.remove("test.txt")
start_time = time.time()
if (rnd == 0):
points = len(df.index) - 1
# Create the SimConnect link
sm = SimConnect()
aq = AircraftRequests(sm, _time=0)
ae = AircraftEvents(sm)
logger.test_simconnect(self, 1)
hsi = Event(b'HEADING_SLOT_INDEX_SET', sm)
hsi(1)
# Check and set initial aircraft settings:
# AP1 ON, ATHR ON, FD ON & CLB
ac_init(aq, ae)
logger.test_init(self, 1)
for i in range(n, points + 1):
if (rnd == 1):
# Random Aircraft situation
if (n == i):
start = n
else:
start = 0
weight, altitude, tas, mach, n1 = data.a32x_state_rnd(
df, start)
else:
weight, altitude, tas, mach, n1 = data.a32x_state_nrm(df, i)
# Set Weight and CG ... this goes first to avoid excessive dumping
W_n_B(aq, weight, cg)
if (i == 1):
logger.test_init(self, 0)
logger.test_loop(self, 1)
logger.test_obj(self, weight, cg, altitude, tas, mach, n1, i,
points)
# Main test point routine - Setting stable aircraft conditions
crz_alt_tas(sm, aq, ae, altitude, tas)
# Altitude & Speed damping "filter". Use VS first as a measure
# of stability
# To avoid excesive damping, fuel and CG are set first with
# enough headroom
# A stability counter is implemented to account for VS damping
counter = 0
prev_n1 = 0
ap_cycler = time.time()
while counter < 50:
if not (round(time.time() - ap_cycler) % 10):
actual_fcu_speed = float(
aq.get("AUTOPILOT_AIRSPEED_HOLD_VAR"))
event_to_trigger = ae.find("AP_MASTER")
if (abs(actual_fcu_speed - tas) > 2):
crz_alt_tas(sm, aq, ae, altitude, tas)
print("FCU Trigger")
if (counter == 0):
print("AP Trigger")
event_to_trigger()
time.sleep(1)
event_to_trigger()
actual_alt = float(aq.get("INDICATED_ALTITUDE"))
actual_tas = float(aq.get("AIRSPEED_TRUE"))
actual_vs = float(aq.get("VERTICAL_SPEED"))
error_alt = round(
abs((actual_alt - altitude) / altitude) * 100, 3)
error_tas = round(abs((actual_tas - tas) / tas) * 100, 3)
if (error_alt < 0.5 and error_tas < 0.5
and abs(actual_vs) < 10):
actual_n1 = aq.get("TURB_ENG_N1:1")
print("Diff N1=" + str(actual_n1 - prev_n1))
if (abs(float(actual_n1) - prev_n1) < 0.1):
counter += 1
print("counter=" + str(counter))
time.sleep(0.1)
else:
counter = 0
prev_n1 = float(actual_n1)
elapsed_time = time.time() - start_time
msg = "Tolerance Figures - Alt: " + str(
error_alt) + "% TAS: " + str(error_tas) + "% VS: " + str(
round(actual_vs,
1)) + "fpm Elapsed Time - " + str(
round(elapsed_time, 2)) + " secs."
self.updateStatus(msg)
QtCore.QCoreApplication.processEvents()
actual_weight = aq.get("TOTAL_WEIGHT")
actual_alt = aq.get("INDICATED_ALTITUDE")
actual_tas = aq.get("AIRSPEED_TRUE")
actual_mach = aq.get("AIRSPEED_MACH")
actual_vs = aq.get("VERTICAL_SPEED")
actual_cg = aq.get("CG_PERCENT")
actual_fn = float(aq.get("TURB_ENG_JET_THRUST:1")) * 2
actual_n1 = aq.get("TURB_ENG_N1:1")
actual_n2 = aq.get("TURB_ENG_N2:1")
actual_n1_cor = aq.get("TURB_ENG_CORRECTED_N1:1")
actual_n2_cor = aq.get("TURB_ENG_CORRECTED_N2:1")
actual_egt_R = float(
aq.get("GENERAL_ENG_EXHAUST_GAS_TEMPERATURE:1"))
actual_egt = (actual_egt_R - 491.67) * 5 / 9
actual_ff = float(
aq.get("TURB_ENG_FUEL_FLOW_PPH:1")) * 2 * 0.453592
logger.test_actual(self, actual_weight, actual_cg, actual_alt,
actual_tas, actual_mach, actual_vs, actual_fn,
actual_n1, actual_n2, actual_n1_cor,
actual_n2_cor, actual_egt, actual_ff, i, points)
time.sleep(0.5)
os.system('copy test.txt test.bck >NUL')
self.dumpToFile()
time.sleep(0.5)
if not (i % 10):
eta = ((time.time() - start_time) / i) * (points - i)
if (eta > 3600):
eta = round(eta / 3600, 2)
subject = "FBW Tester: ETA is " + str(eta) + " hours"
elif (eta < 3600 and eta > 60):
eta = round(eta / 60)
subject = "FBW Tester: ETA is " + str(eta) + " minutes"
else:
eta = eta
subject = "FBW Tester: ETA is " + str(eta) + " seconds"
gmail.gmail(subject)
#sm.quit()
logger.test_loop(self, 0)
logger.test_simconnect(self, 0)
self.dumpToFile()
import sys
def signal_handler(sig, frame):
print('Received SIGINT! Exiting now...')
sm.exit()
sys.exit(0)
signal.signal(signal.SIGINT, signal_handler)
# logging.basicConfig(level=logging.DEBUG)
LOGGER = logging.getLogger(__name__)
LOGGER.info("START")
# time holder for inline commands
ct_g = millis()
# creat simconnection and pass used user classes
sm = SimConnect()
aq = AircraftRequests(sm)
ae = AircraftEvents(sm)
# Add a simple REPL, exposing the SimConnect Interface.
header = "SimConnect Test REPL"
footer = "Closing now!"
# Some Example definitions:
A = aq.find("ATC_ID")
T = ae.find("TOGGLE_PUSHBACK")
H = ae.find("KEY_TUG_HEADING")
S = ae.find("KEY_TUG_SPEED")
def H2I(hdg):
return int((2**32-1)*hdg/360)
def cruise(w, points):
df = fbw.data_read('CRZ')
logger.test_header(w, "CRZ")
start_time = time.time()
i = 1
weight, altitude, ias = fbw.a32x_state(df)
logger.test_env(w, weight, altitude, ias, i, points)
## Create SimConnect link
sm = SimConnect()
aq = AircraftRequests(sm, _time=0)
ae = AircraftEvents(sm)
############################################
## Check Environment and Aircraft Status:
## - AP1 ON, ATHR ON, FD ON
############################################
AP = aq.get("AUTOPILOT_MASTER")
ATHR = aq.get("AUTOTHROTTLE_ACTIVE")
FD = aq.get("AUTOPILOT_FLIGHT_DIRECTOR_ACTIVE")
event_to_trigger = ae.find("TOGGLE_FLIGHT_DIRECTOR")
event_to_trigger()
event_to_trigger()
if (AP == 0):
event_to_trigger = ae.find("AP_MASTER")
event_to_trigger()
if (ATHR == 0):
event_to_trigger = ae.find("AUTO_THROTTLE_ARM")
event_to_trigger()
if (FD == 0):
event_to_trigger = ae.find("TOGGLE_FLIGHT_DIRECTOR")
event_to_trigger()
## Set Throttle to CLIMB
aq.set("GENERAL_ENG_THROTTLE_LEVER_POSITION:1", 82)
aq.set("GENERAL_ENG_THROTTLE_LEVER_POSITION:2", 82)
## Set Key Aircraft Parameters
asi = Event(b'ALTITUDE_SLOT_INDEX_SET', sm)
ssi = Event(b'SPEED_SLOT_INDEX_SET', sm)
## Altitude
target_altitude = int(altitude)
event_to_trigger = ae.find("AP_ALT_VAR_SET_ENGLISH")
event_to_trigger(target_altitude)
asi(1)
aq.set("INDICATED_ALTITUDE", altitude)
## Speed
target_speed = int(ias)
event_to_trigger = ae.find("AP_SPD_VAR_SET")
event_to_trigger(target_speed)
ssi(1)
aq.set("AIRSPEED_INDICATED", ias)
####################################
## Check Altitude/ Speed Stability
####################################
error_alt = 1
error_ias = 1
actual_vs = 1000
while error_alt > 1 or error_ias > 1 or abs(actual_vs) > 20:
actual_alt = aq.get("INDICATED_ALTITUDE")
actual_ias = aq.get("AIRSPEED_INDICATED")
actual_vs = aq.get("VERTICAL_SPEED")
error_alt = abs((actual_alt - altitude) / altitude) * 100
error_ias = abs((actual_ias - ias) / ias) * 100
msg = "Alt: " + str(error_alt) + " IAS: " + str(
error_ias) + " VS: " + str(actual_vs)
w.updateStatus(msg)
#time.sleep(1)
print(error_alt, " ", error_ias, " ", actual_vs)
## Tweak Aircraft Weight
actual_weight = aq.get("TOTAL_WEIGHT")
print(actual_weight)
elapsed_time = time.time() - start_time
#w.statusBar().showMessage("Elapsed= " + str(elapsed_time))
#sm.quit()
exit()
return
import time
from SimConnect import *
sm = SimConnect()
aq = AircraftRequests(sm, _time=0)
ae = AircraftEvents(sm)
# target_speed = 260 #240 - 260
# event_to_trigger = ae.find("AP_SPD_VAR_SET")
# event_to_trigger(target_speed)
# time.sleep(0.5)
# ssi = Event(b'SPEED_SLOT_INDEX_SET', sm)
# ssi(1)
# time.sleep(0.5)
# sm.quit()
# exit()
hsi = Event(b'HEADING_SLOT_INDEX_SET', sm)
hsi(1)
# Check and set initial aircraft settings:
# AP1 ON, ATHR ON, FD ON & CLB
AP = aq.get("AUTOPILOT_MASTER")
ATHR = aq.get("AUTOTHROTTLE_ACTIVE")
FD = aq.get("AUTOPILOT_FLIGHT_DIRECTOR_ACTIVE")
event_to_trigger = ae.find("TOGGLE_FLIGHT_DIRECTOR")
event_to_trigger()
event_to_trigger()
def simconnect_thread_func(threadname):
global simconnect_dict
# Init SimConnect
sm = SimConnect()
aq = AircraftRequests(sm, _time=0)
# Init variables
airborne = False
v_speed_list = []
g_force_list = []
plane_alt_above_ground_list = []
sim_on_ground_list = [1, 1, 1, 1, 1, 1, 1, 1]
run_app = 1
simconnect_dict["G_FORCE"] = 0
simconnect_dict["VERTICAL_SPEED"] = 0
simconnect_dict["SIM_ON_GROUND"] = 0
simconnect_dict["G_FORCE_LANDING"] = "N/A"
simconnect_dict["VERTICAL_SPEED_LANDING"] = "N/A"
simconnect_dict["G_FORCE_LANDING_LIST"] = "N/A"
simconnect_dict["VERTICAL_SPEED_LANDING_LIST"] = "N/A"
simconnect_dict["SIM_ON_GROUND_LIST"] = "N/A"
simconnect_dict["AIRBORNE"] = 0
simconnect_dict["G_FORCE_LIST"] = g_force_list
simconnect_dict["V_SPEED_LIST"] = v_speed_list
simconnect_dict[
"PLANE_ALT_ABOVE_GROUND_LIST"] = plane_alt_above_ground_list
simconnect_dict["LANDING_RATING"] = "N/A"
simconnect_dict["LANDING_COUNTER"] = 0
# Create empty labels for charts
labels_list = []
for i in range(150):
labels_list.append("")
simconnect_dict["LABELS"] = labels_list
# Run Simconnect Calculations
while run_app == 1:
if airborne == True and sum(sim_on_ground_list) == 30:
simconnect_dict["G_FORCE_LANDING"] = max(g_force_list)
max_gforce_index = g_force_list.index(max(g_force_list))
simconnect_dict["VERTICAL_SPEED_LANDING"] = v_speed_list[
max_gforce_index]
simconnect_dict["G_FORCE_LANDING_LIST"] = g_force_list[::-1] * 1
v_speed_list_neg = [elem * (-1) for elem in v_speed_list]
simconnect_dict[
"VERTICAL_SPEED_LANDING_LIST"] = v_speed_list_neg[::-1] * 1
simconnect_dict[
"PLANE_ALT_ABOVE_GROUND_LIST"] = plane_alt_above_ground_list[::
-1] * 1
simconnect_dict[
"LANDING_COUNTER"] = simconnect_dict["LANDING_COUNTER"] + 1
# Landing Rating Based on G-Forces
if simconnect_dict["G_FORCE_LANDING"] < 1.25:
simconnect_dict["LANDING_RATING"] = "Smooth landing"
elif simconnect_dict["G_FORCE_LANDING"] < 1.5:
simconnect_dict["LANDING_RATING"] = "Acceptable landing"
elif simconnect_dict["G_FORCE_LANDING"] < 1.75:
simconnect_dict["LANDING_RATING"] = "Poor landing"
elif simconnect_dict["G_FORCE_LANDING"] < 2:
simconnect_dict["LANDING_RATING"] = "Hard landing"
elif simconnect_dict["G_FORCE_LANDING"] <= 2.5:
simconnect_dict["LANDING_RATING"] = "Very hard landing"
else:
simconnect_dict[
"LANDING_RATING"] = "Structural damage to plane"
airborne = False
if sum(sim_on_ground_list) == 0 and airborne == False:
airborne = True
# Get Current Data
simconnect_dict["G_FORCE"] = round(aq.get("G_FORCE"), 2)
simconnect_dict["VERTICAL_SPEED"] = round(aq.get("VERTICAL_SPEED"))
simconnect_dict["SIM_ON_GROUND"] = aq.get("SIM_ON_GROUND")
simconnect_dict["AIRBORNE"] = airborne
simconnect_dict["G_FORCE_LIST"] = g_force_list
# Make lists
v_speed_list.insert(0, simconnect_dict["VERTICAL_SPEED"])
if len(v_speed_list) > 151:
v_speed_list.pop()
g_force_list.insert(0, simconnect_dict["G_FORCE"])
if len(g_force_list) > 151:
g_force_list.pop()
sim_on_ground_list.insert(0, simconnect_dict["SIM_ON_GROUND"])
if len(sim_on_ground_list) > 31:
sim_on_ground_list.pop()
plane_alt_above_ground_list.insert(
0, (round(aq.get("PLANE_ALT_ABOVE_GROUND"), 1)))
if len(plane_alt_above_ground_list) > 151:
plane_alt_above_ground_list.pop()
def simconnect_thread_func(threadname):
global ui_friendly_dictionary
global event_name
global value_to_use
global sm
global ae
while True:
try:
sm = SimConnect()
print("\n********* MSFS 2020 Mobile Companion App *********\n")
print(f"Local web server for MSFS 2020 Mobile Companion App initialized.\n")
print(
f"Launch {socket.gethostbyname(socket.gethostname())}:4000 in your browser to access MSFS 2020 Mobile Companion App.\n")
print(
f"Make sure your your mobile device is connected to the same local network (WIFI) as this PC.\n")
print(f"Notice: If your computer has more than one active ethernet/WIFI adapter, please check ipconfig in command prompt.\n")
print("**************************************************\n\n")
break
except:
print("Could not find MSFS running. Please launch MSFS first and then restart the MSFS 2020 Mobile Companion App.")
sleep(5)
ae = AircraftEvents(sm)
aq = AircraftRequests(sm)
# Initialize previous altitude for code stability
previous_alt = -400
# Initialize vars for landing info
ui_friendly_dictionary["LANDING_VS1"] = "N/A"
ui_friendly_dictionary["LANDING_T1"] = 0
ui_friendly_dictionary["LANDING_G1"] = "N/A"
ui_friendly_dictionary["LANDING_VS2"] = "N/A"
ui_friendly_dictionary["LANDING_T2"] = 0
ui_friendly_dictionary["LANDING_G2"] = "N/A"
ui_friendly_dictionary["LANDING_VS3"] = "N/A"
ui_friendly_dictionary["LANDING_T3"] = 0
ui_friendly_dictionary["LANDING_G3"] = "N/A"
def thousandify(x):
return f"{x:,}"
async def ui_dictionary(ui_friendly_dictionary, previous_alt, landing_t1, landing_vs1, landing_t2, landing_vs2, landing_t3, landing_vs3, landing_g1, landing_g2, landing_g3):
# Position
try:
ui_friendly_dictionary["LATITUDE"] = round(await aq.get("PLANE_LATITUDE"), 6)
ui_friendly_dictionary["LONGITUDE"] = round(await aq.get("PLANE_LONGITUDE"), 6)
ui_friendly_dictionary["MAGNETIC_COMPASS"] = round(round(await aq.get("PLANE_HEADING_DEGREES_TRUE"), 2) * 180/3.1416, 2)
# ui_friendly_dictionary["MAGVAR"] = round(await aq.get("MAGVAR"))
except:
None
# Radios
ui_friendly_dictionary["NAV1_STANDBY"] = round(await aq.get("NAV_STANDBY_FREQUENCY:1"), 2)
ui_friendly_dictionary["NAV1_ACTIVE"] = round(await aq.get("NAV_ACTIVE_FREQUENCY:1"), 2)
ui_friendly_dictionary["NAV2_STANDBY"] = round(await aq.get("NAV_STANDBY_FREQUENCY:2"), 2)
ui_friendly_dictionary["NAV2_ACTIVE"] = round(await aq.get("NAV_ACTIVE_FREQUENCY:2"), 2)
# ADF Active
adf_use_bcd = int(await aq.get("ADF_ACTIVE_FREQUENCY:1"))
adf_use_digits = ""
for i in reversed(range(4)):
adf_use_digit = math.floor(adf_use_bcd / (65536*(16**i)))
adf_use_digits = adf_use_digits + str(adf_use_digit)
adf_use_bcd = adf_use_bcd - (65536*(16**i)) * adf_use_digit
try:
ui_friendly_dictionary["ADF_USE_1000"] = adf_use_digits[0]
ui_friendly_dictionary["ADF_USE_100"] = adf_use_digits[1]
ui_friendly_dictionary["ADF_USE_10"] = adf_use_digits[2]
ui_friendly_dictionary["ADF_USE_1"] = adf_use_digits[3]
ui_friendly_dictionary["ADF_USE"] = int(adf_use_digits)
except:
None
# ADF Standby
adf_stby = int(await aq.get("ADF_STANDBY_FREQUENCY:1"))/1000
try:
if adf_stby >= 1000:
ui_friendly_dictionary["ADF_STBY_1000"] = str(adf_stby)[0]
ui_friendly_dictionary["ADF_STBY_100"] = str(adf_stby)[1]
ui_friendly_dictionary["ADF_STBY_10"] = str(adf_stby)[2]
ui_friendly_dictionary["ADF_STBY_1"] = str(adf_stby)[3]
else:
ui_friendly_dictionary["ADF_STBY_1000"] = "0"
ui_friendly_dictionary["ADF_STBY_100"] = str(adf_stby)[0]
ui_friendly_dictionary["ADF_STBY_10"] = str(adf_stby)[1]
ui_friendly_dictionary["ADF_STBY_1"] = str(adf_stby)[2]
except:
None
# NAV/ADF Compass Settings
# ui_friendly_dictionary["NAV1_OBS_DEG"] = round(await aq.get("NAV_OBS:1"),0)
# ui_friendly_dictionary["ADF_CARD_DEG"] = round(await aq.get("ADF_CARD"),0)
# ui_friendly_dictionary["NAV2_OBS_DEG"] = round(await aq.get("NAV_OBS:2"),0)
# Comms
ui_friendly_dictionary["COM1_STANDBY"] = round(await aq.get("COM_STANDBY_FREQUENCY:1"), 3)
ui_friendly_dictionary["COM1_ACTIVE"] = round(await aq.get("COM_ACTIVE_FREQUENCY:1"), 3)
ui_friendly_dictionary["COM1_TRANSMIT"] = await aq.get("COM_TRANSMIT:1")
ui_friendly_dictionary["COM2_STANDBY"] = round(await aq.get("COM_STANDBY_FREQUENCY:2"), 3)
ui_friendly_dictionary["COM2_ACTIVE"] = round(await aq.get("COM_ACTIVE_FREQUENCY:2"), 3)
ui_friendly_dictionary["COM2_TRANSMIT"] = await aq.get("COM_TRANSMIT:2")
# XPNDR
xpndr_bcd = await aq.get("TRANSPONDER_CODE:1")
xpndr_digits = ""
# XPNDR Conversion from BCD to Decimal
try:
for i in reversed(range(4)):
xpndr_digit = math.floor(xpndr_bcd / (16**i))
xpndr_digits = xpndr_digits + str(xpndr_digit)
xpndr_bcd = xpndr_bcd - (16**i) * xpndr_digit
except:
None
try:
ui_friendly_dictionary["XPNDR_1000"] = xpndr_digits[0]
ui_friendly_dictionary["XPNDR_100"] = xpndr_digits[1]
ui_friendly_dictionary["XPNDR_10"] = xpndr_digits[2]
ui_friendly_dictionary["XPNDR_1"] = xpndr_digits[3]
ui_friendly_dictionary["XPNDR"] = int(xpndr_digits)
except:
None
# Autopilot
ui_friendly_dictionary["AUTOPILOT_MASTER"] = await aq.get("AUTOPILOT_MASTER")
ui_friendly_dictionary["AUTOPILOT_NAV1_LOCK"] = await aq.get("AUTOPILOT_NAV1_LOCK")
ui_friendly_dictionary["AUTOPILOT_HEADING_LOCK"] = await aq.get("AUTOPILOT_HEADING_LOCK")
ui_friendly_dictionary["AUTOPILOT_ALTITUDE_LOCK"] = await aq.get("AUTOPILOT_ALTITUDE_LOCK")
ui_friendly_dictionary["AUTOPILOT_GLIDESLOPE_HOLD"] = await aq.get("AUTOPILOT_GLIDESLOPE_HOLD")
ui_friendly_dictionary["AUTOPILOT_APPROACH_HOLD"] = await aq.get("AUTOPILOT_APPROACH_HOLD")
ui_friendly_dictionary["AUTOPILOT_BACKCOURSE_HOLD"] = await aq.get("AUTOPILOT_BACKCOURSE_HOLD")
ui_friendly_dictionary["AUTOPILOT_VERTICAL_HOLD"] = await aq.get("AUTOPILOT_VERTICAL_HOLD")
ui_friendly_dictionary["AUTOPILOT_FLIGHT_LEVEL_CHANGE"] = await aq.get("AUTOPILOT_FLIGHT_LEVEL_CHANGE")
ui_friendly_dictionary["AUTOPILOT_AUTOTHROTTLE"] = await aq.get("AUTOTHROTTLE_ACTIVE")
ui_friendly_dictionary["AUTOPILOT_YAW_DAMPER"] = await aq.get("AUTOPILOT_YAW_DAMPER")
ui_friendly_dictionary["AIRSPEED_INDICATED"] = round(await aq.get("AIRSPEED_INDICATED"))
ui_friendly_dictionary["AUTOPILOT_AIRSPEED_HOLD"] = await aq.get("AUTOPILOT_AIRSPEED_HOLD")
# ui_friendly_dictionary["AUTOPILOT_MACH_HOLD_VAR"] = round(await aq.get("AUTOPILOT_MACH_HOLD_VAR"),2)
ui_friendly_dictionary["PLANE_HEADING_DEGREES"] = round(round(await aq.get("PLANE_HEADING_DEGREES_MAGNETIC"), 2) * 180/3.1416, 0)
# Placeholders - Not Actively Used for stress testing
# ui_friendly_dictionary["DA62_DEICE_PUMP"] = await aq.get("MobiFlight.DA62_DEICE_PUMP")
# ui_friendly_dictionary["DA62_ICE_LIGHT_MAX_STATE_ENABLED"] = await aq.get("MobiFlight.DA62_ICE_LIGHT_MAX_STATE_ENABLED")
# ui_friendly_dictionary["JFARROW_AP_HDG"] = await aq.get("MobiFlight.JFARROW_AP_HDG")
# ui_friendly_dictionary["AUTOPILOT_WING_LEVELER"] = await aq.get("AUTOPILOT_WING_LEVELER")
# ui_friendly_dictionary["AUTOPILOT_PITCH_HOLD"] = await aq.get("AUTOPILOT_PITCH_HOLD")
# ui_friendly_dictionary["AUTOPILOT_PITCH_HOLD_REF"] = await aq.get("AUTOPILOT_PITCH_HOLD_REF")
ui_friendly_dictionary["AUTOPILOT_FLIGHT_DIRECTOR_ACTIVE"] = await aq.get("AUTOPILOT_FLIGHT_DIRECTOR_ACTIVE")
# Lights
#ui_friendly_dictionary["LIGHT_LANDING"] = await aq.get("LIGHT_LANDING")
#ui_friendly_dictionary["LIGHT_TAXI"] = await aq.get("LIGHT_TAXI")
#ui_friendly_dictionary["LIGHT_STROBE"] = await aq.get("LIGHT_STROBE")
#ui_friendly_dictionary["LIGHT_NAV"] = await aq.get("LIGHT_NAV")
#ui_friendly_dictionary["LIGHT_BEACON"] = await aq.get("LIGHT_BEACON")
#ui_friendly_dictionary["LIGHT_CABIN"] = await aq.get("LIGHT_CABIN")
#ui_friendly_dictionary["LIGHT_LOGO"] = await aq.get("LIGHT_LOGO")
#ui_friendly_dictionary["LIGHT_PANEL"] = await aq.get("LIGHT_PANEL")
#ui_friendly_dictionary["LIGHT_WING"] = await aq.get("LIGHT_WING")
#ui_friendly_dictionary["LIGHT_RECOGNITION"] = await aq.get("LIGHT_RECOGNITION")
# Pitot Heat and Deice
#ui_friendly_dictionary["PITOT_HEAT"] = await aq.get("PITOT_HEAT")
# ui_friendly_dictionary["PROP_DEICE_SWITCH"] = await aq.get("PROP_DEICE_SWITCH:1")
#ui_friendly_dictionary["ENG_ANTI_ICE"] = await aq.get("ENG_ANTI_ICE:1")
# ui_friendly_dictionary["GEN_ENG_ANTI_ICE"] = await aq.get("GENERAL_ENG_ANTI_ICE_POSITION:1")
#ui_friendly_dictionary["STRUCTURAL_DEICE_SWITCH"] = await aq.get("STRUCTURAL_DEICE_SWITCH")
# ui_friendly_dictionary["PANEL_ANTI_ICE_SWITCH"] = await aq.get("PANEL_ANTI_ICE_SWITCH")
# Sim Rate
ui_friendly_dictionary["SIMULATION_RATE"] = await aq.get("SIMULATION_RATE")
# GPS Next Waypoint
ui_friendly_dictionary["NEXT_WP_LAT"] = await aq.get("GPS_WP_NEXT_LAT")
ui_friendly_dictionary["NEXT_WP_LON"] = await aq.get("GPS_WP_NEXT_LON")
# Other
ui_friendly_dictionary["GEAR_POSITION"] = await aq.get("GEAR_POSITION:1")
ui_friendly_dictionary["FLAPS_HANDLE_PERCENT"] = round(await aq.get("FLAPS_HANDLE_PERCENT")*100)
ui_friendly_dictionary["SPOILERS_ARMED"] = await aq.get("SPOILERS_HANDLE_POSITION")
# Current altitude
current_alt = await aq.get("INDICATED_ALTITUDE")
if current_alt > -300:
ui_friendly_dictionary["INDICATED_ALTITUDE"] = round(current_alt)
previous_alt = current_alt
else:
try:
ui_friendly_dictionary["INDICATED_ALTITUDE"] = previous_alt
except:
pass
# LOC and APPR Mode
try:
if (ui_friendly_dictionary["AUTOPILOT_APPROACH_HOLD"] == 1 and ui_friendly_dictionary["AUTOPILOT_GLIDESLOPE_HOLD"] == 1):
ui_friendly_dictionary["AUTOPILOT_APPR_MODE"] = 1
else:
ui_friendly_dictionary["AUTOPILOT_APPR_MODE"] = 0
if (ui_friendly_dictionary["AUTOPILOT_APPROACH_HOLD"] == 1 and ui_friendly_dictionary["AUTOPILOT_GLIDESLOPE_HOLD"] == 0):
ui_friendly_dictionary["AUTOPILOT_LOC_MODE"] = 1
else:
ui_friendly_dictionary["AUTOPILOT_LOC_MODE"] = 0
except:
None
# Other
current_landing = round(await aq.get("PLANE_TOUCHDOWN_NORMAL_VELOCITY") * 60)
current_time = datetime.datetime.now().strftime('%H:%M:%S')
# Calculate Custom G-Force based on vertical speed
# Model uses Harvsine acceleration model for peak acceleration https://www.nhtsa.gov/sites/nhtsa.dot.gov/files/18esv-000501.pdf
# For time a custom function is used that ranges from 0.25 for GA to 0.35 for airliners. This simulates the rigidness of suspention.
try:
plane_weight = await aq.get("TOTAL_WEIGHT")
except:
plane_weight = 0
plane_weight_adj = max(round(plane_weight * 0.45), 200)
custom_g_force_impact_duration = 0.355 + (-0.103/(1 + (plane_weight_adj/15463)**1.28))
if landing_vs1 != current_landing:
# Move 2nd to 3rd
landing_t3 = landing_t2
landing_vs3 = landing_vs2
landing_g3 = landing_g2
# Move 1st to 2nd
landing_t2 = landing_t1
landing_vs2 = landing_vs1
landing_g2 = landing_g1
# Assign new 1st
landing_t1 = current_time
landing_vs1 = current_landing
landing_g1 = round(1 + (((2 * (current_landing / (60 * 3.281))) / custom_g_force_impact_duration) / 9.80665), 2)
# Dictionary Output
ui_friendly_dictionary["LANDING_VS1"] = landing_vs1
ui_friendly_dictionary["LANDING_T1"] = landing_t1
ui_friendly_dictionary["LANDING_G1"] = landing_g1
ui_friendly_dictionary["LANDING_VS2"] = landing_vs2
ui_friendly_dictionary["LANDING_T2"] = landing_t2
ui_friendly_dictionary["LANDING_G2"] = landing_g2
ui_friendly_dictionary["LANDING_VS3"] = landing_vs3
ui_friendly_dictionary["LANDING_T3"] = landing_t3
ui_friendly_dictionary["LANDING_G3"] = landing_g3
while True:
asyncio.run(ui_dictionary(ui_friendly_dictionary, previous_alt, ui_friendly_dictionary["LANDING_T1"], ui_friendly_dictionary["LANDING_VS1"], ui_friendly_dictionary["LANDING_T2"], ui_friendly_dictionary["LANDING_VS2"], ui_friendly_dictionary["LANDING_T3"], ui_friendly_dictionary["LANDING_VS3"], ui_friendly_dictionary["LANDING_G1"], ui_friendly_dictionary["LANDING_G2"], ui_friendly_dictionary["LANDING_G3"]))
client.publish(topic, value)
LOGGER.debug(topic + " = " + str(value))
client = mqtt.Client()
client.on_connect = on_connect
client.on_message = on_message
client.connect("192.168.89.52", 1883, 60)
client.publish("/FS/CONNECTION", "CONNECTED")
"""Logging settings"""
logging.basicConfig(level=logging.DEBUG)
LOGGER = logging.getLogger(__name__)
LOGGER.info("START")
"""Simconnect Settings"""
sm = SimConnect()
aq = AircraftRequests(sm)
ae = AircraftEvents(sm)
"""Datasets"""
request_lights = [
'LIGHT_STROBE', 'LIGHT_PANEL', 'LIGHT_LANDING', 'LIGHT_TAXI',
'LIGHT_BEACON', 'LIGHT_NAV', 'LIGHT_WING'
]
toggle_plane = [
'SMOKE_TOGGLE',
'GEAR_TOGGLE',
'PITOT_HEAT_TOGGLE',
'PARKING_BRAKES',
]
def main_app(offline: bool):
sm = None
aq = None
ae = None
if not offline:
sm = SimConnect()
aq = AircraftRequests(sm, _time=200)
ae = AircraftEvents(sm)
outport = mido.open_output('X-TOUCH MINI 1')
control_change_dict = {}
note_dict = {}
def event(name: str):
print(f"{name}")
def create_partial(name: str):
return partial(event, name)
def handle_message(msg: mido.Message):
# print(msg)
if msg.type == 'control_change':
if msg.control in control_change_dict:
control_change_dict[msg.control].on_cc_data(msg.value)
elif msg.type == 'note_on':
if msg.note in note_dict:
note_dict[msg.note].on_note_data(True)
elif msg.type == 'note_off':
if msg.note in note_dict:
note_dict[msg.note].on_note_data(False)
inport = mido.open_input('X-TOUCH MINI 0', callback=handle_message)
encoders = []
buttons = []
faders = []
for e in range(1, 17):
encoder = RotaryEncoder(e, outport)
encoders.append(encoder)
for b in range(1, 33):
btn = PushButton(b, outport)
buttons.append(btn)
for f in range(1, 3):
fader = Fader(f)
faders.append(fader)
c = ConfigFile(encoders, buttons, faders, ae)
c.configure()
triggers = c.triggers
for encoder in encoders:
control_change_dict[encoder.rotary_control_channel] = encoder
note_dict[encoder.button_note] = encoder
for btn in buttons:
note_dict[btn.button_note] = btn
for f in faders:
control_change_dict[f.control_channel] = f
triggers[0].on_simvar_data(1.0)
objs = buttons + encoders + triggers
while True:
for obj in objs:
if obj.bound_simvar and aq:
sv = aq.get(obj.bound_simvar)
obj.on_simvar_data(sv)
time.sleep(0.1)
def get_pyfirmata(settings):
return pyfirmata.util.Iterator(pyfirmata.Arduino(settings["comm_port"]))
if __name__ == "__main__":
logging.basicConfig(level=logging.DEBUG)
LOGGER = logging.getLogger(__name__)
LOGGER.info("Program Start")
LOGGER.info("Simulation Setup")
settings = get_settings()
arduinoBoard = get_pyfirmata(settings)
simulation = SimConnect()
aircraftEvents = AircraftEvents(simulation)
aircraftRequests = AircraftRequests(simulation)
inputs = []
LOGGER.info("Simulation Setup")
for pin in settings["pins"]:
inputs.append(
Pins(
arduinoBoard.get_pin(pin["input_type"] + ":" +
pin["pin_number"] + ":" + "i"),
pin["can_repeat"], pin["timeout"], pin["max_value"],
pin["threshold"], pin["compare"],
pin["min_value"], pin["starting_value"],
aircraftEvents.find(pin["function"]), pin["inputType"]))
def on_created(self, event):
print("\nFile created: '{}'.".format(event.src_path))
# Check if sim is running (https://stackoverflow.com/a/7788702)
if not 'FlightSimulator.exe' in (p.name()
for p in psutil.process_iter()):
print(
'Warning: The simulator is not running. Not going to add GPS data to this file.'
)
return
# Connect to sim
print('Getting data from sim..')
sm = SimConnect()
aq = AircraftRequests(sm)
# Get data from sim
data = {
'GPSLatitude': round(aq.get("GPS_POSITION_LAT"), 5), # degrees
'GPSLongitude': round(aq.get("GPS_POSITION_LON"), 5), # degrees
'GPSAltitude': round(aq.get('GPS_POSITION_ALT'), 2), # meter
'GPSSpeed': aq.get('GPS_GROUND_SPEED') # m/s
}
# Disconnect from sim
sm.exit()
# Check if player is not in flight
if round(data['GPSLatitude'], 2) < 0.1 and round(
data['GPSLongitude'], 2) < 0.1 and data['GPSSpeed'] < 0.1:
print(
'Warning: It looks like the player is in a menu. Not going to add GPS data to this file.'
)
return
# Set additional tags (https://exiftool.org/TagNames/GPS.html)
data['GPSLatitudeRef'] = 'North'
if data['GPSLatitude'] < 0:
data['GPSLatitudeRef'] = 'South'
data['GPSLongitudeRef'] = 'East'
if data['GPSLongitude'] < 0:
data['GPSLongitudeRef'] = 'West'
data['GPSAltitudeRef'] = 'Above Sea Level'
data['GPSSpeed'] = round(data['GPSSpeed'] * 3.6,
2) # Convert m/s to km/h
data['GPSSpeedRef'] = 'km/h' # Set unit to km/h
# Compile exiftool command
cmdline = [exiftool]
for key, value in data.items():
if value == -999999:
print('Warning: invalid value for {}: {}.'.format(key, value))
continue
cmdline.append('-{}={}'.format(key, value))
if OVERWRITE:
cmdline.append('-overwrite_original')
if DEBUG:
cmdline.append('-verbose')
cmdline.append(event.src_path)
if DEBUG:
import json
print('data:', json.dumps(data, indent=4))
print(cmdline)
# Add GPS data to screenshot
print('Adding EXIF data to image..')
process = subprocess.Popen(cmdline,
stdin=subprocess.PIPE,
stdout=subprocess.PIPE)
process.communicate(input=b'\n') # Pass exiftool's '-- press ENTER --'
print('Finished. Watching for changes..')
self.process(event)
def simconnect_thread_func(threadname):
global simconnect_dict
# Init SimConnect
sm = SimConnect()
aq = AircraftRequests(sm, _time=0)
# Init variables
airborne = False
g_force = 0
v_speed = 0
plane_alt_above_ground = 0
sim_on_ground = 0
g_force_prev = 0
v_speed_prev = 0
plane_alt_above_ground_prev = 0
lat_prev = 0
lng_prev = 0
bearing_prev = 0
sim_on_ground_prev = 0
v_speed_list_all = []
g_force_list_all = []
v_speed_list = []
g_force_list = []
plane_alt_above_ground_list = []
v_speed_list_ground = []
g_force_list_ground = []
plane_alt_above_ground_list_ground = []
sim_on_ground_list = [1, 1, 1, 1, 1, 1, 1, 1]
run_app = 1
simconnect_dict["G_FORCE"] = 0
simconnect_dict["MAX_G_FORCE"] = 0
simconnect_dict["VERTICAL_SPEED"] = 0.0
simconnect_dict["HORIZONTAL_SPEED"] = 0.0
simconnect_dict["LATITUDE"] = 0.0
simconnect_dict["LONGITUDE"] = 0.0
simconnect_dict["PLANE_ALTITUDE"] = 0.0
simconnect_dict["PLANE_BEARING"] = 0.0
simconnect_dict["PLANE_PITCH_DEGREES"] = 0.0
simconnect_dict["PLANE_BANK_DEGREES"] = 0.0
simconnect_dict["SIM_ON_GROUND"] = 0
simconnect_dict["G_FORCE_LANDING"] = "N/A"
simconnect_dict["VERTICAL_SPEED_LANDING"] = "N/A"
simconnect_dict["SIM_ON_GROUND_LIST"] = "N/A"
simconnect_dict["AIRBORNE"] = 0
simconnect_dict["ENGINE_TYPE"] = -1
simconnect_dict["G_FORCE_LIST"] = g_force_list
simconnect_dict["V_SPEED_LIST"] = v_speed_list
simconnect_dict["G_FORCE_LANDING_LIST"] = "N/A"
simconnect_dict["G_FORCE_LANDING_LIST_GROUND"] = "N/A"
simconnect_dict["VERTICAL_SPEED_LANDING_LIST"] = "N/A"
simconnect_dict["VERTICAL_SPEED_LANDING_LIST_GROUND"] = "N/A"
simconnect_dict[
"PLANE_ALT_ABOVE_GROUND_LIST"] = plane_alt_above_ground_list
simconnect_dict[
"PLANE_ALT_ABOVE_GROUND_LIST_GROUND"] = plane_alt_above_ground_list_ground
simconnect_dict["LANDING_RATING"] = "N/A"
simconnect_dict["LANDING_COUNTER"] = 0
# Create empty labels for charts
labels_list = []
for i in range(150):
labels_list.append("")
simconnect_dict["LABELS"] = labels_list
# Run Simconnect Calculations
while run_app == 1:
# Get Current Data
# Fix for -999999 values
max_g = round(aq.get("MAX_G_FORCE"), 2)
engine = aq.get("ENGINE_TYPE")
v_speed = round(aq.get("VERTICAL_SPEED"), 2)
z_speed = round(aq.get("VELOCITY_WORLD_Z"), 3)
x_speed = round(aq.get("VELOCITY_WORLD_X"), 3)
alt = aq.get("PLANE_ALTITUDE")
gndAlt = aq.get("PLANE_ALT_ABOVE_GROUND")
grnd_elv = round(alt - gndAlt, 0)
dist = aq.get("GPS_WP_DISTANCE") * 0.539957
grnd_speed = math.sqrt((z_speed * z_speed) +
(x_speed * x_speed)) * 0.592484
grnd_speed = round(grnd_speed, 2)
true_speed = round(aq.get("AIRSPEED_TRUE"), 2)
indi_speed = round(aq.get("AIRSPEED_INDICATED"), 2)
mach_speed = round(aq.get("AIRSPEED_MACH"), 3)
lat = aq.get("PLANE_LATITUDE")
if lat < -99999:
lat = lat_prev
else:
lat_prev = lat
lng = aq.get("PLANE_LONGITUDE")
if lng < -99999:
lng = lng_prev
else:
lng_prev = lng
bearing = aq.get("PLANE_HEADING_DEGREES_TRUE")
if bearing < -99999:
bearing = bearing_prev
else:
bearing_prev = bearing
if v_speed < -99999:
v_speed = v_speed_prev
else:
g_force_custom = (round(aq.get("ACCELERATION_WORLD_Y")) / 32.2) + 1
v_speed_prev = v_speed
g_force = round(aq.get("G_FORCE"), 2)
if g_force < -99999:
g_force = g_force_prev
else:
g_force_prev = g_force
plane_alt_above_ground = round(aq.get("PLANE_ALT_ABOVE_GROUND"), 1)
if plane_alt_above_ground < -99999:
plane_alt_above_ground = plane_alt_above_ground_prev
else:
plane_alt_above_ground_prev = plane_alt_above_ground
sim_on_ground = aq.get("SIM_ON_GROUND")
if sim_on_ground < -99999:
sim_on_ground = sim_on_ground_prev
else:
sim_on_ground_prev = sim_on_ground
# Make lists
sim_on_ground_list.insert(0, sim_on_ground)
if len(sim_on_ground_list) > 31:
sim_on_ground_list.pop()
v_speed_list_all.insert(0, v_speed)
if len(v_speed_list_all) > 151:
v_speed_list_all.pop()
g_force_list_all.insert(0, g_force)
if len(g_force_list_all) > 151:
g_force_list_all.pop()
# Make lists for graph - separation between airborne and landing
if sim_on_ground == 1:
v_speed_list.insert(0, "null")
if len(v_speed_list) > 151:
v_speed_list.pop()
g_force_list.insert(0, "null")
if len(g_force_list) > 151:
g_force_list.pop()
plane_alt_above_ground_list.insert(0, "null")
if len(plane_alt_above_ground_list) > 151:
plane_alt_above_ground_list.pop()
v_speed_list_ground.insert(0, v_speed)
if len(v_speed_list_ground) > 151:
v_speed_list_ground.pop()
g_force_list_ground.insert(0, g_force)
if len(g_force_list_ground) > 151:
g_force_list_ground.pop()
plane_alt_above_ground_list_ground.insert(0,
plane_alt_above_ground)
if len(plane_alt_above_ground_list_ground) > 151:
plane_alt_above_ground_list_ground.pop()
else:
v_speed_list.insert(0, v_speed)
if len(v_speed_list) > 151:
v_speed_list.pop()
g_force_list.insert(0, g_force)
if len(g_force_list) > 151:
g_force_list.pop()
plane_alt_above_ground_list.insert(0, plane_alt_above_ground)
if len(plane_alt_above_ground_list) > 151:
plane_alt_above_ground_list.pop()
v_speed_list_ground.insert(0, "null")
if len(v_speed_list_ground) > 151:
v_speed_list_ground.pop()
g_force_list_ground.insert(0, "null")
if len(g_force_list_ground) > 151:
g_force_list_ground.pop()
plane_alt_above_ground_list_ground.insert(0, "null")
if len(plane_alt_above_ground_list_ground) > 151:
plane_alt_above_ground_list_ground.pop()
# Populate vars to JSON dictionary
simconnect_dict["ENGINE_TYPE"] = engine
simconnect_dict["G_FORCE"] = g_force
simconnect_dict["MAX_G_FORCE"] = max_g
simconnect_dict["VERTICAL_SPEED"] = v_speed
simconnect_dict["HORIZONTAL_SPEED"] = true_speed
simconnect_dict["INDICATED_SPEED"] = indi_speed
simconnect_dict["MACH_SPEED"] = mach_speed
simconnect_dict["GRND_SPEED"] = grnd_speed
simconnect_dict["LATITUDE"] = round(lat, 7)
simconnect_dict["LONGITUDE"] = round(lng, 7)
simconnect_dict["BEARING"] = math.degrees(bearing)
simconnect_dict["ALTITUDE"] = round(alt, 1)
simconnect_dict["GND_ALTITUDE"] = round(plane_alt_above_ground, 1)
simconnect_dict["GRND_ELEV"] = grnd_elv
simconnect_dict["SIM_ON_GROUND"] = sim_on_ground
simconnect_dict["AIRBORNE"] = airborne
simconnect_dict["TARGET_DIST"] = round(dist / 1000, 2)
# Make landing/airborne decision
if airborne == True and sum(sim_on_ground_list) == 30:
# Fix - need to get the last value before on ground readings
v_speed_list_touchdown = v_speed_list_ground
g_force_list_touchdown = g_force_list_ground
change_last = False
for idx, element in enumerate(v_speed_list_touchdown):
if idx >= 1:
if element == 0 and v_speed_list_touchdown[idx - 1] == 1:
if change_last == False:
v_speed_list_touchdown[idx] = v_speed_list[idx]
g_force_list_touchdown[idx] = g_force_list[idx]
change_last = True
else:
change_last = False
else:
change_last = False
v_speed_list_touchdown = [
0 if x == "null" else x for x in v_speed_list_touchdown
]
g_force_list_touchdown = [
0 if x == "null" else x for x in g_force_list_touchdown
]
simconnect_dict["G_FORCE_LANDING"] = max(g_force_list_touchdown)
simconnect_dict["VERTICAL_SPEED_LANDING"] = min(
v_speed_list_touchdown)
# Create Lists for Graphs
simconnect_dict["G_FORCE_LANDING_LIST"] = g_force_list[::-1] * 1
simconnect_dict[
"G_FORCE_LANDING_LIST_GROUND"] = g_force_list_ground[::-1] * 1
v_speed_list_neg = [
elem * (-1) if elem != "null" else "null"
for elem in v_speed_list
]
v_speed_list_ground_neg = [
elem * (-1) if elem != "null" else "null"
for elem in v_speed_list_ground
]
simconnect_dict[
"VERTICAL_SPEED_LANDING_LIST"] = v_speed_list_neg[::-1] * 1
simconnect_dict[
"VERTICAL_SPEED_LANDING_LIST_GROUND"] = v_speed_list_ground_neg[::
-1] * 1
simconnect_dict[
"PLANE_ALT_ABOVE_GROUND_LIST"] = plane_alt_above_ground_list[::
-1] * 1
simconnect_dict[
"PLANE_ALT_ABOVE_GROUND_LIST_GROUND"] = plane_alt_above_ground_list_ground[::
-1] * 1
simconnect_dict[
"LANDING_COUNTER"] = simconnect_dict["LANDING_COUNTER"] + 1
# Landing Rating Based on G-Forces
if simconnect_dict["VERTICAL_SPEED_LANDING"] > -60:
simconnect_dict["LANDING_RATING"] = "Very soft landing"
elif simconnect_dict["VERTICAL_SPEED_LANDING"] > -120:
simconnect_dict["LANDING_RATING"] = "Soft landing"
elif simconnect_dict["VERTICAL_SPEED_LANDING"] > -200:
simconnect_dict["LANDING_RATING"] = "Average landing"
elif simconnect_dict["VERTICAL_SPEED_LANDING"] > -300:
simconnect_dict["LANDING_RATING"] = "Firm landing"
elif simconnect_dict["VERTICAL_SPEED_LANDING"] > -400:
simconnect_dict["LANDING_RATING"] = "Hard landing"
elif simconnect_dict["VERTICAL_SPEED_LANDING"] > -600:
simconnect_dict["LANDING_RATING"] = "Very hard landing"
else:
simconnect_dict[
"LANDING_RATING"] = "Structural damage to plane"
airborne = False
if sum(sim_on_ground_list) == 0 and airborne == False:
airborne = True
def cruise(self):
rnd = self.radioButton.isChecked()
points = int(self.linePoints.text())
random.seed(int(self.lineSeed.text()))
cg = float(self.lineCG.text()) / 100
error_alt = 1000
error_tas = 1000
actual_vs = 1000
limit_alt = float(self.lineAltErr.text())
limit_tas = float(self.lineTASErr.text())
limit_vs = float(self.lineVSErr.text())
inFile = "data/" + self.lineInFile.text()
clb = float(self.lineCLB.text())
n = 1
# Read the Aircraft Data file
df = data.data_read('CRZ', inFile)
logger.test_header(self, "CRZ")
if os.path.exists(self.lineOutFile.text()):
os.remove(self.lineOutFile.text())
start_time = time.time()
if (rnd == False):
points = len(df.index) - 1
# Create the SimConnect link
sm = SimConnect()
aq = AircraftRequests(sm, _time=0)
ae = AircraftEvents(sm)
logger.test_simconnect(self, 1)
hsi = Event(b'HEADING_SLOT_INDEX_SET', sm)
hsi(1)
# Check and set initial aircraft settings:
# AP1 ON, ATHR ON, FD ON & CLB
ac_init(aq, ae, clb)
logger.test_init(self, 1)
for i in range(n, points + 1):
if (rnd == True):
# Random Aircraft situation
if (n == i):
start = n
else:
start = 0
weight, altitude, tas, mach, n1 = data.a32x_state_rnd(
df, start)
else:
weight, altitude, tas, mach, n1 = data.a32x_state_nrm(df, i)
# Set Weight and CG ... this goes first to avoid excessive dumping
W_n_B(aq, weight, cg)
if (i == 1):
logger.test_init(self, 0)
logger.test_loop(self, 1)
logger.test_obj(self, weight, cg, altitude, tas, mach, n1, i,
points)
# Main test point routine - Setting stable aircraft conditions
crz_alt_tas(sm, aq, ae, altitude, tas)
# Altitude & Speed damping "filter". Use VS first as a measure
# of stability
# To avoid excesive damping, fuel and CG are set first with
# enough headroom
# A stability counter is implemented to account for VS damping
counter = 0 # 0 - initial, 1 - within the loop, 10 - outside the loop
previous = []
minimums = []
maximums = []
averages = []
step = 0 # 0 - none, 1 - one found, 2 - two found
increment = -1 # -1 - Initial, 0 - decreasing, 1 - increasing
ap_cycler = time.time()
while counter < 10:
if not (round(time.time() - ap_cycler) % 10):
actual_fcu_speed = float(
aq.get("AUTOPILOT_AIRSPEED_HOLD_VAR"))
event_to_trigger = ae.find("AP_MASTER")
if (abs(actual_fcu_speed - tas) > 2):
crz_alt_tas(sm, aq, ae, altitude, tas)
# #print("FCU Trigger")
# if (counter == 0):
# #print("AP Trigger")
# event_to_trigger()
# time.sleep(1)
# event_to_trigger()
actual_alt = float(aq.get("INDICATED_ALTITUDE"))
actual_tas = float(aq.get("AIRSPEED_TRUE"))
actual_vs = float(aq.get("VERTICAL_SPEED"))
error_alt = round(
abs((actual_alt - altitude) / altitude) * 100, 3)
error_tas = round(abs((actual_tas - tas) / tas) * 100, 3)
# Stability has been reached
if (error_alt < limit_alt and error_tas < limit_tas
and abs(actual_vs) < limit_vs):
actual_n1 = float(aq.get("TURB_ENG_N1:1"))
actual_n2 = float(aq.get("TURB_ENG_N2:1"))
actual_n1_cor = float(aq.get("TURB_ENG_CORRECTED_N1:1"))
actual_n2_cor = float(aq.get("TURB_ENG_CORRECTED_N2:1"))
actual_fn = float(aq.get("TURB_ENG_JET_THRUST:1")) * 2
actual_egt_R = float(
aq.get("GENERAL_ENG_EXHAUST_GAS_TEMPERATURE:1"))
actual_ff = float(aq.get("TURB_ENG_FUEL_FLOW_PPH:1"))
# First pass
if (counter == 0):
previous = [
actual_n1, actual_n2, actual_n1_cor, actual_n2_cor,
actual_fn, actual_egt_R, actual_ff
]
counter = 1
#print("start")
# Looking for a Maximum
#print(actual_n1)
if (actual_n1 > previous[0]):
if (increment != 0): # If not swtiching
maximums = [
actual_n1, actual_n2, actual_n1_cor,
actual_n2_cor, actual_fn, actual_egt_R,
actual_ff
]
previous = [
actual_n1, actual_n2, actual_n1_cor,
actual_n2_cor, actual_fn, actual_egt_R,
actual_ff
]
else:
minimums = previous
#print("minimum")
step += 1
if (step == 2):
counter += 10
else:
previous = [
actual_n1, actual_n2, actual_n1_cor,
actual_n2_cor, actual_fn, actual_egt_R,
actual_ff
]
increment = 1
else:
if (increment != 1): # If not swtiching
minimums = [
actual_n1, actual_n2, actual_n1_cor,
actual_n2_cor, actual_fn, actual_egt_R,
actual_ff
]
previous = [
actual_n1, actual_n2, actual_n1_cor,
actual_n2_cor, actual_fn, actual_egt_R,
actual_ff
]
else:
maximums = previous
#print("maximum")
step += 1
if (step == 2):
counter += 10
else:
previous = [
actual_n1, actual_n2, actual_n1_cor,
actual_n2_cor, actual_fn, actual_egt_R,
actual_ff
]
increment = 0
time.sleep(0.5)
else:
counter = 0 # 0 - initial, 1 - within the loop, 10 - outside the loop
previous = []
minimums = []
maximums = []
averages = []
step = 0 # 0 - none, 1 - one found, 2 - two found
increment = -1 # -1 - Initial, 0 - decreasing, 1 - increasing
elapsed_time = time.time() - start_time
msg = "Tolerance Figures - Alt: " + str(
error_alt) + "% TAS: " + str(error_tas) + "% VS: " + str(
round(actual_vs,
1)) + "fpm Elapsed Time - " + str(
round(elapsed_time, 2)) + " secs."
self.updateStatus(msg)
QtCore.QCoreApplication.processEvents()
a = minimums[0] + ((maximums[0] - minimums[0]) / 2)
print("Max= " + str(maximums[0]) + " Min= " + str(minimums[0]) +
" Avg= " + str(a))
actual_weight = aq.get("TOTAL_WEIGHT")
actual_alt = aq.get("INDICATED_ALTITUDE")
actual_tas = aq.get("AIRSPEED_TRUE")
actual_mach = aq.get("AIRSPEED_MACH")
actual_vs = aq.get("VERTICAL_SPEED")
actual_cg = aq.get("CG_PERCENT")
actual_n1 = minimums[0] + ((maximums[0] - minimums[0]) / 2)
actual_n2 = minimums[1] + ((maximums[1] - minimums[1]) / 2)
actual_n1_cor = minimums[2] + ((maximums[2] - minimums[2]) / 2)
actual_n2_cor = minimums[3] + ((maximums[3] - minimums[3]) / 2)
actual_fn = minimums[4] + ((maximums[4] - minimums[4]) / 2)
actual_egt_R = minimums[5] + ((maximums[5] - minimums[5]) / 2)
actual_ff = (minimums[6] +
((maximums[6] - minimums[6]) / 2)) * 2 * 0.453592
actual_egt = (actual_egt_R - 491.67) * 5 / 9
logger.test_actual(self, actual_weight, actual_cg, actual_alt,
actual_tas, actual_mach, actual_vs, actual_fn,
actual_n1, actual_n2, actual_n1_cor,
actual_n2_cor, actual_egt, actual_ff, i, points)
time.sleep(0.5)
os.system('copy ' + self.lineOutFile.text() + ' test.bck >NUL')
self.dumpToFile()
time.sleep(0.5)
if not (i % 10):
eta = ((time.time() - start_time) / i) * (points - i)
if (eta > 3600):
eta = round(eta / 3600, 2)
subject = "FBW Tester: ETA is " + str(eta) + " hours"
elif (eta < 3600 and eta > 60):
eta = round(eta / 60)
subject = "FBW Tester: ETA is " + str(eta) + " minutes"
else:
eta = eta
subject = "FBW Tester: ETA is " + str(eta) + " seconds"
outFile = self.lineOutFile.text()
gmail.gmail(subject, outFile)
#sm.quit()
logger.test_loop(self, 0)
logger.test_simconnect(self, 0)
self.dumpToFile()
def init_simconnect(self):
self.sc = SimConnect()
self.aircraftReqs = AircraftRequests(self.sc, _time=0)
self.aircraftEvents = AircraftEvents(self.sc)
def test_no_default_attributes_in_init(self):
sm = create_autospec(SimConnect.SimConnect)
pl = SimConnect.Plane(sm=sm, add_default=False)
with self.assertRaises(AttributeError):
pl.altitude