def get_day_flyability(self, ground, day):
day_flyability = {}
weather_slices = WeatherTimeSlice.objects.filter(day_of_occurance=day)
if empty(weather_slices):
raise UnflyableError("No weather time slices")
for wts in weather_slices:
wts_time,flyability = self.get_wts_flyability(ground, wts)
day_flyability[wts_time]=flyability
if logger:
logger.debug("Flyability for day %s: %s" % (day.id, day_flyability))
if empty(day_flyability):
raise UnflyableError("Empty day_flyability")
return day_flyability
def get_landing_conditions(self, check_day):
landing_list = list(Landing.objects.filter(site=self))
if empty(landing_list):
raise UnflyableError("No landings for site %s" %self)
if logger:
logger.debug("Landing list is %s" % landing_list)
logger.debug("Flyable landings with %s site on %s day" % (self,check_day))
return self.get_ground_conditions(landing_list, check_day)
def get_ground_conditions(self, ground_list, check_day):
ground_status = {}
for ground in ground_list:
ground_status[ground] = self.get_day_flyability(ground, check_day)
if logger:
logger.debug( "Ground check for the %s ground at %s" % (ground.name, ground.site))
if logger:
logger.debug("Resultant ground status dict: %s" % (ground_status))
if empty(ground_status.iteritems()):
raise UnflyableError("Ground status has no statuses")
else:
return ground_status
class chessboard(object):
global row,column,pos_hash,empty
pos_hash={}
empty=empty()
def __init__(self, arg,arg1):
super(chessboard, self).__init__()
self.row = arg
self.column= arg1
self.x = [[empty for i in range(self.row)] for j in range(self.column)]
self.display()
def pos(self,row,col,char,player):
self.x[row][col]=char
print(self.x[row][col].position,char.name)
pos_hash[char.name]=[row,col]
def display(self):
for i in range(self.row):
for t in range(self.column):
sys.stdout.write(" "+self.x[i][t].name)
print("\n")
def valid(self,pos):
if(pos[0]<=self.row-1 and pos[0]>=0 and pos[1]<=self.column-1 and pos[1]>=0):
return True
else:
return False
def find_char(self,char):
if char in pos_hash:
pos=pos_hash[char]
if(self.x[pos[0]][pos[1]].name==" - "):
del pos_hash[char]
return False
else:
return self.x[pos[0]][pos[1]]
else:
print("It is dead ! Get over it")
return False
def conseq(self,conseq,player):
for i in conseq:
x=self.x
print("value of iter",x)
if(x[i[0]][i[1]].player!=player and x[i[0]][i[1]].player!=None):
x[i[0]][i[1]].alive=False
x[i[0]][i[1]]=empty
def emptyy(self,row,col):
self.x[row][col]=empty
wing.sref = 31.00 wing.span = 34.10 wing.mac = wing.sref / wing.span wing.Nwr = 2 * 41 + 22 wing.deltaw = (wing.span**2) / (wing.Nwr * wing.sref) wing.t_c = 0.128 wing.Nwer = 10. horizontal.area = 10. #FAKE NUMBER!!!!! horizontal.span = wing.sref * ((1. + 3. / 16.) / 9.) horizontal.mac = horizontal.area / horizontal.span horizontal.Nwr = 16. horizontal.deltah = (horizontal.span**2) / (horizontal.Nwr * horizontal.area) horizontal.t_c = 0.12 # I have no idea vertical.area = 10. #FAKE NUMBER!!!!! vertical.span = wing.sref * ((11. / 16.) / 9.) vertical.mac = horizontal.area / horizontal.span vertical.Nwr = 10. vertical.deltah = (vertical.span**2) / (vertical.Nwr * vertical.area) vertical.t_c = 0.12 # I have no idea aircraft.nult = 1.75 aircraft.gw = 109633.3 / 1000. aircraft.qm = 28.87 aircraft.Ltb = wing.sref * ((2. + 1. / 8.) / 9.) weights = empty.empty(wing, aircraft, horizontal, vertical) #print weights
wing.sref = 31.00 wing.span = 34.10 wing.mac = wing.sref/wing.span wing.Nwr = 2*41+22 wing.deltaw = (wing.span**2)/(wing.Nwr*wing.sref) wing.t_c = 0.128 wing.Nwer = 10. horizontal.area = 10. #FAKE NUMBER!!!!! horizontal.span = wing.sref*((1.+3./16.)/9.) horizontal.mac = horizontal.area/horizontal.span horizontal.Nwr = 16. horizontal.deltah = (horizontal.span**2)/(horizontal.Nwr*horizontal.area) horizontal.t_c = 0.12 # I have no idea vertical.area = 10. #FAKE NUMBER!!!!! vertical.span = wing.sref*((11./16.)/9.) vertical.mac = horizontal.area/horizontal.span vertical.Nwr = 10. vertical.deltah = (vertical.span**2)/(vertical.Nwr*vertical.area) vertical.t_c = 0.12 # I have no idea aircraft.nult = 1.75 aircraft.gw = 109633.3/1000. aircraft.qm = 28.87 aircraft.Ltb = wing.sref*((2.+1./8.)/9.) weights = empty.empty(wing,aircraft,horizontal,vertical) #print weights
