Ejemplo n.º 1
0
		#p2.Draw('')
		p.Draw('cont4z')

		#p2.GetXaxis().SetRangeUser(0,1)
		# gPad.Update()
		# palette = exclusion.GetListOfFunctions().FindObject("palette")
		# palette.SetX1NDC(1.1)
		# palette.SetX2NDC(1.2)
		# palette.SetY1NDC(1.1)
		# palette.SetY2NDC(1.2)
		#p.Write()
		#plots.append(p)
	

		if tipo=='obs':
			bm = c.GetBottomMargin()
			lm = c.GetLeftMargin()
			rm = c.GetRightMargin()
			to = c.GetTopMargin()
			x1 = p.GetXaxis().GetXmin()
			yf = p.GetYaxis().GetXmin()
			x2 = p.GetXaxis().GetXmax()
			y2 = p.GetYaxis().GetXmax()

			Xa = (x2-x1)/(1-lm-rm)-(x2-x1)
			Ya = (y2-yf)/(1-bm-to)-(y2-yf)
			LM = Xa*(lm/(lm+rm))
			RM = Xa*(rm/(lm+rm))
			BM = Ya*(bm/(bm+to))
			TM = Ya*(to/(bm+to))
			null2 = TPad("null2","",0,0,1,1)
leg3 = TLegend(0.7, 0.65, 0.88, 0.89)
leg3.SetBorderSize(0)
leg3.AddEntry(h[4], "STop_s", "f")
leg3.AddEntry(h[5], "STop_t", "f")
leg3.AddEntry(h[6], "STop_tbar", "f")
leg3.AddEntry(h[8], "STop_tbarW", "f")
leg3.AddEntry(h[7], "STop_tW", "f")

# set stytle
H = cv.GetWh()
W = cv.GetWw()
l = cv.GetLeftMargin()
t = cv.GetTopMargin()
r = cv.GetRightMargin()
b = cv.GetBottomMargin()

lumiText = str(lumi) + " fb^{-1} (13 TeV)"
lumiTextSize = 0.5
lumiTextOffset = 0.2

cmsText = "CMS"
cmsTextFont = 61
cmsTextSize = 0.75
cmsTextOffset = 0.1

extraText = "Preliminary"
extraTextFont = 52
extraOverCmsTextSize = 0.76

relPosX = 0.045
Ejemplo n.º 3
0
		#p2.Draw('')
		p.Draw('cont4z')
		#p2.GetXaxis().SetRangeUser(0,1)
		# gPad.Update()
		# palette = exclusion.GetListOfFunctions().FindObject("palette")
		# palette.SetX1NDC(1.1)
		# palette.SetX2NDC(1.2)
		# palette.SetY1NDC(1.1)
		# palette.SetY2NDC(1.2)
		#p.Write()
		#plots.append(p)
		xx=array('d',[-0.05,1.05,1.05])
		yy=array('d',[1.05,1.05,-0.05])
	

		bm = c.GetBottomMargin()
   		lm = c.GetLeftMargin()
   		rm = c.GetRightMargin()
   		to = c.GetTopMargin()
   		x1 = p.GetXaxis().GetXmin()
   		yf = p.GetYaxis().GetXmin()
   		x2 = p.GetXaxis().GetXmax()
   		y2 = p.GetYaxis().GetXmax()

   		Xa = (x2-x1)/(1-lm-rm)-(x2-x1)
   		Ya = (y2-yf)/(1-bm-to)-(y2-yf)
   		LM = Xa*(lm/(lm+rm))
   		RM = Xa*(rm/(lm+rm))
   		BM = Ya*(bm/(bm+to))
   		TM = Ya*(to/(bm+to))