ISCE_INSAR/components/isceobj/InsarProc/runSetmocomppath.py

124 lines
4.9 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
logger = logging.getLogger('isce.insar.runSetmocomppath')
def averageHeightAboveElp(planet, peg, orbit):
elp = planet.get_elp()
elp.setSCH(peg.latitude, peg.longitude, peg.heading)
t, posXYZ, velXYZ, offset = orbit._unpackOrbit()
hsum = 0.
for xyz in posXYZ:
llh = elp.xyz_to_llh(xyz)
hsum += llh[2]
print("averageHeightAboveElp: hsum, len(posXYZ), havg = ",
hsum, len(posXYZ), havg)
return hsum/len(posXYZ)
def sVelocityAtMidOrbit(planet, peg, orbit):
elp = planet.get_elp()
elp.setSCH(peg.latitude, peg.longitude, peg.heading)
t, posXYZ, velXYZ, offset = orbit._unpackOrbit()
sch, vsch = elp.xyzdot_to_schdot(
posXYZ[len(posXYZ)/2+1], velXYZ[len(posXYZ)/2+1])
print("sVelocityAtPeg: len(posXYZ)/2., vsch = ",
len(posXYZ)/2+1, vsch)
return vsch[0]
def runSetmocomppath(self, peg=None):
from isceobj.Location.Peg import Peg
from stdproc.orbit.pegManipulator import averagePeg
from isceobj.Catalog import recordInputsAndOutputs
logger.info("Selecting individual peg points")
planet = self._insar.getReferenceFrame().getInstrument().getPlatform().getPlanet()
referenceOrbit = self._insar.getReferenceOrbit()
secondaryOrbit = self._insar.getSecondaryOrbit()
if peg:
self._insar.setPeg(peg)
logger.info("Using the given peg = %r", peg)
self._insar.setFirstAverageHeight(
averageHeightAboveElp(planet, peg, referenceOrbit))
self._insar.setSecondAverageHeight(
averageHeightAboveElp(planet, peg, secondaryOrbit))
self._insar.setFirstProcVelocity(
sVelocityAtMidOrbit(planet, peg, referenceOrbit))
self._insar.setSecondProcVelocity(
sVelocityAtMidOrbit(planet, peg, secondaryOrbit))
return
pegpts = []
for orbitObj, order in zip((referenceOrbit, secondaryOrbit)
,('First', 'Second')):
objGetpeg = stdproc.createGetpeg()
if peg:
objGetpeg.setPeg(peg)
objGetpeg.wireInputPort(name='planet', object=planet)
objGetpeg.wireInputPort(name='Orbit', object=orbitObj)
self._stdWriter.setFileTag("getpeg", "log")
self._stdWriter.setFileTag("getpeg", "err")
self._stdWriter.setFileTag("getpeg", "out")
objGetpeg.setStdWriter(self._stdWriter)
logger.info('Peg points are computed for individual SAR scenes.')
objGetpeg.estimatePeg()
pegpts.append(objGetpeg.getPeg())
recordInputsAndOutputs(self._insar.procDoc, objGetpeg, "getpeg", \
logger, "runSetmocomppath")
#Piyush
# I set these values here for the sake of continuity, but they need to be updated
# in orbit2sch as the correct peg point is not yet known
getattr(self._insar,'set%sAverageHeight'%(order))(objGetpeg.getAverageHeight())
getattr(self._insar,'set%sProcVelocity'%(order))(objGetpeg.getProcVelocity())
logger.info('Combining individual peg points.')
peg = averagePeg(pegpts, planet)
if self.pegSelect.upper() == 'REFERENCE':
logger.info('Using reference info for peg point')
self._insar.setPeg(pegpts[0])
elif self.pegSelect.upper() == 'SECONDARY':
logger.info('Using secondary infor for peg point')
self._insar.setPeg(pegpts[1])
elif self.pegSelect.upper() == 'AVERAGE':
logger.info('Using average peg point')
self._insar.setPeg(peg)
else:
raise Exception('Unknown peg selection method')