Use "chart" rather than "table".

airpower/aircraft.py

@@ -442,15 +442,15 @@ def startmove(self, flighttype, powerap, actions):
     if not isinstance(powerap, (int, float)) or powerap < 0 or powerap % 0.5 != 0:
       raise ValueError("invalid power AP %s" % powerap)
     # TODO: Don't assume CL.
-    powertable = self._aircrafttype.powertable("CL")
+    powerchart = self._aircrafttype.powerchart("CL")
     if powerap == 0:
       powersetting = "NOR"
-    elif powerap <= powertable["MIL"]:
+    elif powerap <= powerchart["MIL"]:
       powersetting = "MIL"
-    elif "AB" in powertable and powerap <= powertable["AB"]:
+    elif "AB" in powerchart and powerap <= powerchart["AB"]:
       powersetting = "AB"
     else:
-      raise ValueError("requested power %s exceeds aircraft capability.")
+      raise ValueError("requested power %s APs exceeds aircraft capability.")
 
     self._restore(apturn.turn() - 1)
 
@@ -548,7 +548,8 @@ def _endmove(self):
           turnap = 0.0
         else:
           # TODO: Don't assume CL.
-          turnap = -self._aircrafttype.turndragtable("CL")[self._maxturnrate]
+          # TODO: Calculate this at the moment of the maximum turn, since it depends on the configuration.
+          turnap = -self._aircrafttype.turndragchart("CL")[self._maxturnrate]
 
       self._report("power    APs = %+.1f." % self._powerap)
       self._report("turn     APs = %+.1f and %+.1f." % (turnap, self._sustainedturnap))

airpower/aircrafttype.py

@@ -3,7 +3,7 @@ class aircrafttype:
   def __init__(self, name):
     self._name = name
 
-  def powertable(self, configuration):
+  def powerchart(self, configuration):
     if self._name == "F-80C":
       return {
         "CL" : { "MIL": 1.0, },
@@ -17,7 +17,7 @@ def powertable(self, configuration):
         "DT" : { "MIL": 0.5, },
       }[configuration]    
 
-  def turndragtable(self, configuration):
+  def turndragchart(self, configuration):
     if self._name == "F-80C":
       return {
         "CL" : { "TT": 0.0, "HT": 1.0, "BT": 1.0, },