#airlift01
#JDN oct 2024

import matplotlib.pyplot as plt 
import numpy as np
 
 
vrs = "\n-----\nairlift v0.9\n--"
  
#air pres to altitude
# file holds altitide in meter
datafile = 'src/data/shield1/LOG00082raw.TXT'
 
# just 1,2,3,4
x = []

#values
accx = [] 
accy = []  
accz = [] 
gyrox = [] 
gyroy = [] 
gyroz = [] 
temp = []  
baro = []  
alt = []  

n = 0 # nr elm
sum = 0 # sum of y values

def readData():
	i=1
	for line in open(datafile, 'r'):
		lines = [i for i in line.split()] 
		accx.append(float(lines[0]))
		accy.append(float(lines[1]))		
		accz.append(float(lines[2]))
		gyrox.append(float(lines[3]))
		gyroy.append(float(lines[4]))
		gyroz.append(float(lines[5]))
		temp.append(float(lines[6]))
		baro.append(float(lines[7]))
		alt.append(float(lines[8]))
		x.append(i)
		i = i+1
	return i
		
def countEl():
	cnt = 0
	for i in accx:
		cnt = cnt+1
	return cnt

def readFile():
	readData()     
	cnt = countEl() 


 	 
def printHeader():
	print(vrs)
	print("\nRAW DUMP \n")
	print("dataset ",datafile)
	print("no of row of elements ",n)
	print("time(sec) ",n)
	  
  
def runit():
	n = readFile()
	printHeader()
	fig,(ax0,ax1,ax2,ax3,ax4,ax5,ax6,ax7,ax8)=plt.subplots(9)			
	ax0.plot(x,accx)
	ax1.plot(x,accy)
	ax2.plot(x,accz)
	ax3.plot(x,gyrox)
	ax4.plot(x,gyroy)
	ax5.plot(x,gyroz)
	ax6.plot(x,temp)
	ax7.plot(x,baro)
	ax8.plot(x,alt)
	plt.show()
 
if __name__ == "__main__":
	runit()