FlightSim-Streaming/XPlaneConnectCSP
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Pre-rollout phase

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This commit is contained in:
cs-powell
2025-03-05 14:28:14 -05:00
parent 2dd880dbed
commit d354655482
1 changed files with 25 additions and 4 deletions
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29
Python3/src/cognitiveModel.py
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@@ -34,7 +34,7 @@ class AircraftLandingModel(pyactr.ACTRModel):
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")
altitude = self.client.getDREF("sim/cockpit2/gauges/indicators/altitude_ft_pilot")
altitude = self.client.getDREF("sim/flightmodel/position/y_agl")
pitch = self.client.getDREF("sim/flightmodel/position/true_theta")
@@ -57,6 +57,11 @@ class AircraftLandingModel(pyactr.ACTRModel):
self.flare = False
self.pitch = pitch[0]
#Rollout Specific Parameters
self.rollOut = False
self.target_airspeed = 80
@@ -188,7 +193,6 @@ class AircraftLandingModel(pyactr.ACTRModel):
rudder, self.integral_heading = self.proportionalIntegralControl(0,self.heading, self.target_heading, self.integral_heading,scaleFactor.SCALERUDDER)
throttle, self.integral_descent_rate = self.proportionalIntegralControl(0,self.descent_rate, self.target_descent_rate, self.integral_descent_rate,scaleFactor.SCALETHROTTLE)
### 1. For Calculated Yoke and Throttle Values
#Invert Throttle Control & divide by 5 to scale
throttle = -throttle
@@ -259,6 +263,10 @@ class AircraftLandingModel(pyactr.ACTRModel):
trimdref = "sim/flightmodel/controls/elv_trim"
trim = 0
self.client.sendDREF(trimdref,trim)
if(self.rollOut):
brakedref = "sim/cockpit2/controls/parking_brake_ratio"
brake = 1
self.client.sendDREF(brakedref,brake)
self.client.sendCTRL([yoke_pull, yoke_steer, rudder, throttle, -998, -998]) # Control inputs: [yoke_pull, yoke_steer, rudder, throttle]
@@ -291,11 +299,24 @@ class AircraftLandingModel(pyactr.ACTRModel):
self.altitude = altitude[0]
self.pitch = pitch[0]
if(self.altitude <= 2500):
##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_rate_rad_sec") #Wheel Rotation Rate
if(self.altitude <= 50):
self.flare = True
self.Ki = 0.1 ## Increase Control Authority to compensate for decreasing airspeed
self.Ki = 0.01 ## Increase Control Authority to compensate for decreasing airspeed
print("Altitude < 500; Flare Set True")
if(wheelWeight > 0 and wheelRate > 0):
#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")
# def rules(self):