Version without any extension tasks attempted

Author: jakb2403

lander/lander.cpp

@@ -19,13 +19,13 @@ void autopilot (void)
 {
   // INSERT YOUR CODE HERE
 
-  // Deploy parachute if lander under 70km and safe to deploy
-  if (parachute_status == NOT_DEPLOYED && safe_to_deploy_parachute() && altitude < 70000){
-    parachute_status = DEPLOYED;
-  }
-  
-  // Enable altitude stabilisation
-  stabilized_attitude = true;
+//  // Deploy parachute if lander under 70km and safe to deploy
+//  if (parachute_status == NOT_DEPLOYED && safe_to_deploy_parachute() && altitude < 70000){
+//    parachute_status = DEPLOYED;
+//  }
+//
+//  // Enable altitude stabilisation
+//  stabilized_attitude = true;
 
   // Calculate error term
   double error = -(0.5 + K_h * altitude + (velocity * position.norm()));
@@ -118,7 +118,7 @@ void initialize_simulation (void)
   scenario_description[3] = "polar launch at escape velocity (but drag prevents escape)";
   scenario_description[4] = "elliptical orbit that clips the atmosphere and decays";
   scenario_description[5] = "descent from 200km";
-  scenario_description[6] = "aerostationary orbit";
+  scenario_description[6] = "";
   scenario_description[7] = "";
   scenario_description[8] = "";
   scenario_description[9] = "";
@@ -194,14 +194,14 @@ void initialize_simulation (void)
     break;
 
   case 6:
-    // a circular equitorial orbit where the period of orbit is the same as the orbital period of Mars on its axis of rotation
-      position = vector3d(20428000.0, 0.0, 0.0);
-      velocity = vector3d(0.0, 1448.155346, 0.0);
-    orientation = vector3d(0.0, 0.0, 90.0);
-    delta_t = 0.1;
-    parachute_status = NOT_DEPLOYED;
-    stabilized_attitude = true;
-    autopilot_enabled = false;
+//    // a circular equitorial orbit where the period of orbit is the same as the orbital period of Mars on its axis of rotation
+//      position = vector3d(20428000.0, 0.0, 0.0);
+//      velocity = vector3d(0.0, 1448.155346, 0.0);
+//    orientation = vector3d(0.0, 0.0, 90.0);
+//    delta_t = 0.1;
+//    parachute_status = NOT_DEPLOYED;
+//    stabilized_attitude = true;
+//    autopilot_enabled = false;
     break;
 
   case 7: