ISCE_INSAR/contrib/stack/topsStack/baselineGrid.py

184 lines
5.8 KiB
Python
Executable File

#!/usr/bin/env python3
# Author: Piyush Agram
# Copyright 2016
#Heresh Fattahi, Adopted for stack
import argparse
import logging
import datetime
import isce
import isceobj
import mroipac
import os
import s1a_isce_utils as ut
def createParser():
parser = argparse.ArgumentParser( description='Use polynomial offsets and create burst by burst interferograms')
parser.add_argument('-m', '--reference', dest='reference', type=str, required=True,
help='Directory with reference acquisition')
parser.add_argument('-s', '--secondary', dest='secondary', type=str, required=True,
help='Directory with secondary acquisition')
parser.add_argument('-b', '--baseline_file', dest='baselineFile', type=str, required=True,
help='An output text file which contains the computed baseline')
return parser
def cmdLineParse(iargs = None):
parser = createParser()
return parser.parse_args(args=iargs)
def getMergedOrbit(product):
from isceobj.Orbit.Orbit import Orbit
###Create merged orbit
orb = Orbit()
orb.configure()
burst = product[0].bursts[0]
#Add first burst orbit to begin with
for sv in burst.orbit:
orb.addStateVector(sv)
for pp in product:
##Add all state vectors
for bb in pp.bursts:
for sv in bb.orbit:
if (sv.time< orb.minTime) or (sv.time > orb.maxTime):
orb.addStateVector(sv)
bb.orbit = orb
return orb
#logger = logging.getLogger('isce.topsinsar.runPreprocessor')
def main(iargs=None):
'''Compute baseline.
'''
inps=cmdLineParse(iargs)
from isceobj.Planet.Planet import Planet
import numpy as np
referenceSwathList = ut.getSwathList(inps.reference)
secondarySwathList = ut.getSwathList(inps.secondary)
swathList = list(sorted(set(referenceSwathList+secondarySwathList)))
#catalog = isceobj.Catalog.createCatalog(self._insar.procDoc.name)
baselineDir = os.path.dirname(inps.baselineFile)
if baselineDir != '':
os.makedirs(baselineDir, exist_ok=True)
referenceswaths = []
secondaryswaths = []
for swath in swathList:
referencexml = os.path.join( inps.reference, 'IW{0}.xml'.format(swath))
secondaryxml = os.path.join( inps.secondary, 'IW{0}.xml'.format(swath))
if os.path.exists(referencexml) and os.path.exists(secondaryxml):
reference = ut.loadProduct(os.path.join(inps.reference , 'IW{0}.xml'.format(swath)))
secondary = ut.loadProduct(os.path.join(inps.secondary , 'IW{0}.xml'.format(swath)))
referenceswaths.append(reference)
secondaryswaths.append(secondary)
refElp = Planet(pname='Earth').ellipsoid
mStartingRange = min([x.startingRange for x in referenceswaths])
mFarRange = max([x.farRange for x in referenceswaths])
mSensingStart = min([x.sensingStart for x in referenceswaths])
mSensingStop = max([x.sensingStop for x in referenceswaths])
mOrb = getMergedOrbit(referenceswaths)
dr = referenceswaths[0].bursts[0].rangePixelSize
dt = referenceswaths[0].bursts[0].azimuthTimeInterval
nPixels = int(np.round( (mFarRange - mStartingRange)/dr)) + 1
nLines = int(np.round( (mSensingStop - mSensingStart).total_seconds() / dt)) + 1
sOrb = getMergedOrbit(secondaryswaths)
rangeLimits = mFarRange - mStartingRange
nRange = int(np.ceil(rangeLimits/7000.))
slantRange = mStartingRange + np.arange(nRange) * rangeLimits / (nRange - 1.0)
azimuthLimits = (mSensingStop - mSensingStart).total_seconds()
nAzimuth = int(np.ceil(azimuthLimits))
azimuthTime = [mSensingStart + datetime.timedelta(seconds= x * azimuthLimits/(nAzimuth-1.0)) for x in range(nAzimuth)]
Bpar = np.zeros(nRange, dtype=np.float32)
Bperp = np.zeros(nRange, dtype=np.float32)
fid = open(inps.baselineFile, 'wb')
print('Baseline file {0} dims: {1}L x {2}P'.format(inps.baselineFile, nAzimuth, nRange))
if inps.reference == inps.secondary:
Bperp = np.zeros((nAzimuth,nRange), dtype=np.float32)
Bperp.tofile(fid)
else:
for ii, taz in enumerate(azimuthTime):
referenceSV = mOrb.interpolate(taz, method='hermite')
mxyz = np.array(referenceSV.getPosition())
mvel = np.array(referenceSV.getVelocity())
for jj, rng in enumerate(slantRange):
target = mOrb.rdr2geo(taz, rng)
targxyz = np.array(refElp.LLH(target[0], target[1], target[2]).ecef().tolist())
slvTime,slvrng = sOrb.geo2rdr(target)
secondarySV = sOrb.interpolateOrbit(slvTime, method='hermite')
sxyz = np.array( secondarySV.getPosition())
aa = np.linalg.norm(sxyz-mxyz)
costheta = (rng*rng + aa*aa - slvrng*slvrng)/(2.*rng*aa)
Bpar[jj] = aa*costheta
perp = aa * np.sqrt(1 - costheta*costheta)
direction = np.sign(np.dot( np.cross(targxyz-mxyz, sxyz-mxyz), mvel))
Bperp[jj] = direction*perp
Bperp.tofile(fid)
fid.close()
####Write XML
img = isceobj.createImage()
img.setFilename( inps.baselineFile)
img.bands = 1
img.scheme = 'BIP'
img.dataType = 'FLOAT'
img.setWidth(nRange)
img.setAccessMode('READ')
img.setLength(nAzimuth)
img.renderHdr()
img.renderVRT()
###Create oversampled VRT file
cmd = 'gdal_translate -of VRT -ot Float32 -r bilinear -outsize {xsize} {ysize} {infile}.vrt {infile}.full.vrt'.format(xsize=nPixels, ysize=nLines, infile=inps.baselineFile)
status = os.system(cmd)
if status:
raise Exception('cmd: {0} Failed'.format(cmd))
if __name__ == '__main__':
'''
Main driver.
'''
main()