FlightSim-Streaming/XPlaneConnectCSP
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middle of major changes for setting location

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cs-powell
2025-03-28 13:16:11 -04:00
parent 411c20098f
commit 1df378d7b1
4 changed files with 82 additions and 108 deletions
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110
Python3/src/cognitiveModel.py
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@@ -284,105 +284,35 @@ class AircraftLandingModel(pyactr.ACTRModel):
#Hit the Brakes
brakedref = "sim/cockpit2/controls/parking_brake_ratio"
brake = 1
self.client.sendDREF(brakedref,brake)
self.client.sendDREF(brakedref,brake)
self.client.sendCTRL([yoke_pull, yoke_steer, rudder, throttle, -998, -998]) # Control inputs: [yoke_pull, yoke_steer, rudder, throttle]
# Update the model's DM based on X-Plane data
def update_aircraft_state(self):
"""
Slower Method
"""
# print("In aircraft state")
# print("Entered Update Aircraft State")
# Retrieve current data from X-Plane
# airspeed = self.client.getDREF("sim/cockpit2/gauges/indicators/airspeed_kts_pilot")
# roll = self.client.getDREF("sim/cockpit2/gauges/indicators/roll_AHARS_deg_pilot")
# heading = self.client.getDREF("sim/cockpit2/gauges/indicators/heading_AHARS_deg_mag_pilot")
# descent_rate = self.client.getDREF("sim/flightmodel/position/vh_ind_fpm")
# altitudeAGL = self.client.getDREF("sim/flightmodel/position/y_agl")
# pitch = self.client.getDREF("sim/flightmodel/position/true_theta")
# brake = self.client.getDREF("sim/cockpit2/controls/parking_brake_ratio")
# wheelS = self.client.getDREF("sim/flightmodel2/gear/tire_rotation_speed_rad_sec")
# wheelW = self.client.getDREF("sim/flightmodel/parts/tire_vrt_def_veh")
# self.airspeed = airspeed[0]
# self.roll = roll[0]
# self.heading = heading[0]
# self.descent_rate = descent_rate[0]
# self.altitude = altitudeAGL[0]
# self.pitch = pitch[0]
# self.wheelSpeed = wheelS[0]
# self.wheelWeight = wheelW[0]
# self.brakes = brake[0]
# #Phase Change Indicator
# wheelWeight = self.client.getDREF("sim/flightmodel/parts/tire_vrt_def_veh") #Strut deflection, Weight on the wheels
# wheelRate = self.client.getDREF("sim/flightmodel2/gear/tire_rotation_speed_rad_sec") #Wheel Rotation Rate
"""
Faster Method
"""
self.getAndLoadDREFS()
def conditionChecks(self):
if(self.wheelWeight > 0.01 and self.wheelSpeed > 1):
#Two Parameters to Confirm Touchdown and wheel contact
# "sim/flightmodel/parts/tire_vrt_def_veh" #Gear Strut Deflection (Weight on wheels)
# "sim/flightmodel2/gear/tire_rotation_rate_rad_sec" #Tire Rotation Rate
self.rollOut = True
print("Hit the brakes")
if(self.altitude <= 20):
self.flare = True
self.Ki = 0.01 ## Increase Control Authority to compensate for decreasing airspeed
print("Altitude < 500; Flare Set True")
if(self.wheelWeight > 0.01 and self.wheelSpeed > 1):
#Two Parameters to Confirm Touchdown and wheel contact
# "sim/flightmodel/parts/tire_vrt_def_veh" #Gear Strut Deflection (Weight on wheels)
# "sim/flightmodel2/gear/tire_rotation_rate_rad_sec" #Tire Rotation Rate
self.rollOut = True
print("Hit the brakes")
# Update the model's DM based on X-Plane data
def update_aircraft_state(self):
"""
Faster Method
"""
self.getAndLoadDREFS()
self.conditionChecks()
# def logData(self):
# def rules(self):
# """
# Define the rules for descent control using proportional-integral control for all controls at once.
# """
# return [
# # Rule to adjust all controls simultaneously based on PI control for each parameter
# pyactr.Production(
# condition=pyactr.Condition("airspeed", "airspeed") &
# pyactr.Condition("roll", "roll") &
# pyactr.Condition("heading", "heading") &
# pyactr.Condition("descent_rate", "descent_rate") &
# pyactr.Condition("target_airspeed", "target_airspeed") &
# pyactr.Condition("target_roll", "target_roll") &
# pyactr.Condition("target_heading", "target_heading") &
# pyactr.Condition("target_descent_rate", "target_descent_rate"),
# action=self.update_controls_simultaneously(),
# ),
# ]
# # Function to get the current dataref value for a given parameter
# def getDref(parameter_name):
# # Depending on the parameter name, you would query X-Plane datarefs
# if parameter_name == "Airspeed":
# # Get airspeed dataref
# return client.getData([DATAREF_AIRSPEED])
# elif parameter_name == "Roll":
# # Get roll angle dataref
# return client.getData([DATAREF_ROLL])
# elif parameter_name == "Hdg":
# # Get heading dataref
# return client.getData([DATAREF_HEADING])
# elif parameter_name == "DescentRate":
# # Get descent rate dataref
# return client.getData([DATAREF_DESCENT_RATE])