FlightSim-Streaming/XPlaneConnectCSP
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Reconnect wrapper v1 complete

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cs-powell
2025-03-29 03:23:26 -04:00
parent 07526ca5a3
commit fc068ef1d0
2 changed files with 231 additions and 145 deletions
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56
Python3/src/cognitiveModel.py
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@@ -29,8 +29,19 @@ class AircraftLandingModel(pyactr.ACTRModel):
brakeDREF = "sim/cockpit2/controls/parking_brake_ratio"
wheelSpeedDREF = "sim/flightmodel2/gear/tire_rotation_speed_rad_sec"
wheelWeightDREF = "sim/flightmodel/parts/tire_vrt_def_veh"
self.sources = [airspeedDREF,rollDREF,magneticHeadingDREF,verticalSpeedDREF,altitudeAGLDREF,pitchDREF,brakeDREF,wheelSpeedDREF,wheelWeightDREF]
# self.sources = [airspeedDREF,rollDREF,magneticHeadingDREF,verticalSpeedDREF,altitudeAGLDREF,pitchDREF,brakeDREF,wheelSpeedDREF,wheelWeightDREF]
self.sources = {
"airspeed" : airspeedDREF,
"roll" : rollDREF,
"heading" : magneticHeadingDREF,
"verticalSpeed" : verticalSpeedDREF,
"altitude": altitudeAGLDREF,
"pitch" : pitchDREF,
"brake": brakeDREF,
"wheelSpeed": wheelSpeedDREF,
"wheelWeight": wheelWeightDREF
}
"""
Initial Initialization of destination Variables and loading into destinations array
"""
@@ -54,8 +65,19 @@ class AircraftLandingModel(pyactr.ACTRModel):
self.brakes = brake[0]
self.wheelSpeed = wheelS[0]
self.wheelWeight = wheelW[0]
self.destinations = [self.airspeed,self.roll,self.heading,self.descent_rate,self.altitude,self.pitch,self.brakes,self.wheelSpeed,self.wheelWeight]
# self.destinations = [self.airspeed,self.roll,self.heading,self.descent_rate,self.altitude,self.pitch,self.brakes,self.wheelSpeed,self.wheelWeight]
self.destinations = {
"airspeed" : self.airspeed,
"roll" : self.roll,
"heading" : self.heading,
"verticalSpeed" : self.descent_rate,
"altitude": self.altitude,
"pitch" : self.pitch,
"brake": self.brakes,
"wheelSpeed": self.wheelSpeed,
"wheelWeight": self.wheelWeight
}
"""
Initial Initialization of target Values
"""
@@ -105,18 +127,26 @@ class AircraftLandingModel(pyactr.ACTRModel):
# while(idx < len(self.sources) - 1):
# self.variableAtlas[0] = [self.sources[idx],self.destinations[idx],self.targets[idx]]
# idx += 1
def reassignClient(self,newClient):
self.client = newClient
def getAndLoadDREFS(self):
results = self.client.getDREFs(self.sources)
results = self.client.getDREFs(self.sources.values())
idx = 0
while(idx < len(results) - 2):
self.destinations[idx] = results[idx][0]
if(idx == 1):
print("getDrefs: " + str(results[idx][0]))
print("current destination: " + str(self.destinations[idx]))
print("current main Airspeed: " + str(self.airspeed))
idx += 1
for key in self.sources:
self.destinations[key] = results[idx]
idx+=1
print("getDrefs: " + str(results[1][0]))
print("current destination: " + str(self.destinations["airspeed"]))
print("current main Airspeed: " + str(self.airspeed))
# while(idx < len(results) - 2):
# self.destinations[idx] = results[idx][0]
# if(idx == 1):
# print("getDrefs: " + str(results[idx][0]))
# print("current destination: " + str(self.destinations[idx]))
# print("current main Airspeed: " + str(self.airspeed))
# idx += 1
def printControls(self,calculated,errors,yokePull,yokeSteer,rudder,throttle):
@@ -129,7 +159,7 @@ class AircraftLandingModel(pyactr.ACTRModel):
# print("*Parameter,Target,Current,Throttle: " + "Descent Rate, " + str(self.target_descent_rate) + "," + str(self.descent_rate)+ "," + str(throttle))
parameter = ["Airspeed","Roll","Heading","Descent Rate","Altitude","Flare: Pitch", "Brakes: Wheel Speed", "Brakes: Wheel Weight"]
target = [str(round(self.target_airspeed)),str(round(self.target_roll)),str(round(self.target_heading,3)),str(round(self.target_descent_rate,3)),str(round(self.altitude,3)),str(round(self.target_pitch,3)),0, 0]
current = [str(round(self.airspeed,3)),str(round(self.roll,3)),str(round(self.heading,3)),str(round(self.descent_rate,3)),str(round(self.altitude,3)),str(round(self.pitch,3)),str(round(self.wheelSpeed,3)),str(round(self.wheelWeight,3))]
current = [str(round(self.destinations["airspeed"],3)),str(round(self.roll,3)),str(round(self.heading,3)),str(round(self.descent_rate,3)),str(round(self.altitude,3)),str(round(self.pitch,3)),str(round(self.wheelSpeed,3)),str(round(self.wheelWeight,3))]
controlVal = [str(round(yokePull,3)),str(round(yokeSteer,3)),str(round(rudder,3)),str(round(throttle,3)),str(round(self.altitude,3)),str(self.flare),str(round(self.brakes,3)),str(round(self.brakes,3))]
header_row = "{:<20} {:<20} {:<20} {:>10}"
@@ -307,7 +337,7 @@ class AircraftLandingModel(pyactr.ACTRModel):
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 and self.airspeed < 1 and self.brakes == 1):
if(self.wheelWeight > 0.01 and self.wheelSpeed > 1 and self.destinations["airspeed"] < 1 and self.brakes == 1):
self.inProgress = False
def simulationStatus(self):