ISCE_INSAR/components/isceobj/InsarProc/runFormSLC.py

185 lines
7.0 KiB
Python

#~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~
# Copyright 2012 California Institute of Technology. ALL RIGHTS RESERVED.
#
# Licensed under the Apache License, Version 2.0 (the "License");
# you may not use this file except in compliance with the License.
# You may obtain a copy of the License at
#
# http://www.apache.org/licenses/LICENSE-2.0
#
# Unless required by applicable law or agreed to in writing, software
# distributed under the License is distributed on an "AS IS" BASIS,
# WITHOUT WARRANTIES OR CONDITIONS OF ANY KIND, either express or implied.
# See the License for the specific language governing permissions and
# limitations under the License.
#
# United States Government Sponsorship acknowledged. This software is subject to
# U.S. export control laws and regulations and has been classified as 'EAR99 NLR'
# (No [Export] License Required except when exporting to an embargoed country,
# end user, or in support of a prohibited end use). By downloading this software,
# the user agrees to comply with all applicable U.S. export laws and regulations.
# The user has the responsibility to obtain export licenses, or other export
# authority as may be required before exporting this software to any 'EAR99'
# embargoed foreign country or citizen of those countries.
#
# Author: Brett George
#~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~
import logging
import stdproc
import isceobj
import pickle
from isceobj.Util.decorators import use_api
logger = logging.getLogger('isce.insar.runFormSLC')
#Run FormSLC for reference
def reference(self, deltaf=None):
from isceobj.Catalog import recordInputsAndOutputs
from iscesys.ImageUtil.ImageUtil import ImageUtil as IU
v,h = self.insar.vh()
objRaw = self.insar.rawReferenceIQImage.clone()
objRaw.accessMode = 'read'
objFormSlc = stdproc.createFormSLC(name='insarapp_formslc_reference')
objFormSlc.setBodyFixedVelocity(v)
objFormSlc.setSpacecraftHeight(h)
objFormSlc.setAzimuthPatchSize(self.patchSize)
objFormSlc.setNumberValidPulses(self.goodLines)
objFormSlc.setNumberPatches(self.numPatches)
objFormSlc.setLookSide(self.insar._lookSide)
objFormSlc.setNumberAzimuthLooks(self.insar.numberAzimuthLooks)
logger.info("Focusing Reference image")
objFormSlc.stdWriter = self.stdWriter
if (deltaf is not None) and (objFormSlc.azimuthResolution is None):
ins = self.insar.referenceFrame.getInstrument()
prf = ins.getPulseRepetitionFrequency()
res = ins.getPlatform().getAntennaLength() / 2.0
azbw = min(v/res, prf)
res = v/azbw
factor = 1.0 - (abs(deltaf)/azbw)
logger.info('REFERENCE AZIMUTH BANDWIDTH FACTOR = %f'%(factor))
azres = res / factor
#jng This is a temporary solution seems it looks that same banding problem
#can be resolved by doubling the azres. The default azResFactor is still one.
objFormSlc.setAzimuthResolution(azres*self.insar.azResFactor)
####newInputs
objSlc = objFormSlc(rawImage=objRaw,
orbit=self.insar.referenceOrbit,
frame=self.insar.referenceFrame,
planet=self.insar.referenceFrame.instrument.platform.planet,
doppler=self.insar.dopplerCentroid,
peg=self.insar.peg)
imageSlc = isceobj.createSlcImage()
IU.copyAttributes(objSlc, imageSlc)
imageSlc.setAccessMode('read')
objSlc.finalizeImage()
objRaw.finalizeImage()
recordInputsAndOutputs(self.insar.procDoc, objFormSlc,
"runFormSLC.reference", logger, "runFormSLC.reference")
logger.info('New Width = %d'%(imageSlc.getWidth()))
self.insar.referenceSlcImage = imageSlc
self.insar.formSLC1 = objFormSlc
return objFormSlc.numberPatches
#Run FormSLC on secondary
def secondary(self, deltaf=None):
from isceobj.Catalog import recordInputsAndOutputs
from iscesys.ImageUtil.ImageUtil import ImageUtil as IU
v,h = self.insar.vh()
objRaw = self.insar.rawSecondaryIQImage.clone()
objRaw.accessMode = 'read'
objFormSlc = stdproc.createFormSLC(name='insarapp_formslc_secondary')
objFormSlc.setBodyFixedVelocity(v)
objFormSlc.setSpacecraftHeight(h)
objFormSlc.setAzimuthPatchSize(self.patchSize)
objFormSlc.setNumberValidPulses(self.goodLines)
objFormSlc.setNumberPatches(self.numPatches)
objFormSlc.setNumberAzimuthLooks(self.insar.numberAzimuthLooks)
objFormSlc.setLookSide(self.insar._lookSide)
logger.info("Focusing Reference image")
objFormSlc.stdWriter = self.stdWriter
if (deltaf is not None) and (objFormSlc.azimuthResolution is None):
ins = self.insar.secondaryFrame.getInstrument()
prf = ins.getPulseRepetitionFrequency()
res = ins.getPlatform().getAntennaLength()/2.0
azbw = min(v / res, prf)
res = v / azbw
factor = 1.0 - (abs(deltaf) / azbw)
logger.info('SECONDARY AZIMUTH BANDWIDTH FACTOR = %f'%(factor))
azres = res/factor
objFormSlc.setAzimuthResolution(azres)
objSlc = objFormSlc(rawImage=objRaw,
orbit=self.insar.secondaryOrbit,
frame=self.insar.secondaryFrame,
planet=self.insar.secondaryFrame.instrument.platform.planet,
doppler=self.insar.dopplerCentroid,
peg=self.insar.peg)
imageSlc = isceobj.createSlcImage()
IU.copyAttributes(objSlc, imageSlc)
imageSlc.setAccessMode('read')
objSlc.finalizeImage()
objRaw.finalizeImage()
recordInputsAndOutputs(self.insar.procDoc, objFormSlc,
"runFormSLC.secondary", logger, "runFormSLC.secondary")
logger.info('New Width = %d'%(imageSlc.getWidth()))
self.insar.secondarySlcImage = imageSlc
self.insar.formSLC2 = objFormSlc
return objFormSlc.numberPatches
@use_api
def runFormSLC(self):
mDoppler = self.insar.referenceDoppler.getDopplerCoefficients(inHz=True)
sDoppler = self.insar.secondaryDoppler.getDopplerCoefficients(inHz=True)
deltaf = abs(mDoppler[0] - sDoppler[0])
n_reference = reference(self, deltaf=deltaf)
n_secondary = secondary(self, deltaf=deltaf)
self.insar.setNumberPatches(min(n_reference, n_secondary))
self.is_mocomp = int(
(self.insar.formSLC1.azimuthPatchSize -
self.insar.formSLC1.numberValidPulses)/2
)
self.insar.is_mocomp = self.is_mocomp
self.insar.patchSize = self.insar.formSLC1.azimuthPatchSize
self.insar.numberValidPulses = self.insar.formSLC1.numberValidPulses
logger.info('Number of Valid Pulses = %d'%(self.insar.numberValidPulses))
return None
###PSA - for testing
def wgs84_to_sch(orbit, peg, pegHavg, planet):
'''
Convert WGS84 orbits to SCH orbits and return it.
'''
import stdproc
from iscesys.StdOEL.StdOELPy import create_writer
import copy
stdWriter = create_writer("log","",True,filename='orb.log')
orbSch = stdproc.createOrbit2sch(averageHeight=pegHavg)
orbSch.setStdWriter(stdWriter)
orbSch(planet=planet, orbit=orbit, peg=peg)
schOrigOrbit = copy.copy(orbSch.orbit)
return schOrigOrbit