From cb46f259fe82a59ddfe33f1a5727444733a4fafa Mon Sep 17 00:00:00 2001
From: cs-powell <142438185+cs-powell@users.noreply.github.com>
Date: Mon, 24 Feb 2025 16:40:14 -0500
Subject: [PATCH] preliminary descent and basic flare Python Client
 testplatform.py & cognitiveModel.py

---
 Python3/src/cognitiveModel.py | 11 ++++++-----
 1 file changed, 6 insertions(+), 5 deletions(-)

diff --git a/Python3/src/cognitiveModel.py b/Python3/src/cognitiveModel.py
index 14ae401..988387f 100644
--- a/Python3/src/cognitiveModel.py
+++ b/Python3/src/cognitiveModel.py
@@ -51,8 +51,9 @@ class AircraftLandingModel(pyactr.ACTRModel):
 
         # Integral gains (tune these values for performance)
         self.Kp = 0.1  # Proportional gain
-        # self.Ki = 0.01  # Integral gain
-        self.Ki = 0.001  # Integral gain
+        # self.Ki = 0.01  # Integral gain                
+        self.Ki = 0  # Integral gain
+
 
 
     def printControls(self,calculated,errors,yokePull,yokeSteer,rudder,throttle):
@@ -164,16 +165,16 @@ class AircraftLandingModel(pyactr.ACTRModel):
 
         throttle = 0.15
 
-        if(self.altitude < 350): ## Integrate using the control equations;; A goal state update
+        if(self.altitude < 100): ## Integrate using the control equations;; A goal state update
             throttle = 0.1
             yoke_pull = 0.3
 
 
-        if(self.altitude < 200): ## Integrate using the control equations;; A goal state update
+        if(self.altitude < 70): ## Integrate using the control equations;; A goal state update
             throttle = 0.05
             yoke_pull = 0.4
 
-        if(self.altitude < 150): ## Integrate using the control equations;; A goal state update
+        if(self.altitude < 50): ## Integrate using the control equations;; A goal state update
             throttle = 0
             yoke_pull = 0.4