80 lines
3.3 KiB
Python
80 lines
3.3 KiB
Python
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#~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~
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# Copyright 2013 California Institute of Technology. ALL RIGHTS RESERVED.
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#
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# Licensed under the Apache License, Version 2.0 (the "License");
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# you may not use this file except in compliance with the License.
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# You may obtain a copy of the License at
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#
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# http://www.apache.org/licenses/LICENSE-2.0
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#
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# Unless required by applicable law or agreed to in writing, software
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# distributed under the License is distributed on an "AS IS" BASIS,
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# WITHOUT WARRANTIES OR CONDITIONS OF ANY KIND, either express or implied.
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# See the License for the specific language governing permissions and
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# limitations under the License.
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#
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# United States Government Sponsorship acknowledged. This software is subject to
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# U.S. export control laws and regulations and has been classified as 'EAR99 NLR'
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# (No [Export] License Required except when exporting to an embargoed country,
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# end user, or in support of a prohibited end use). By downloading this software,
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# the user agrees to comply with all applicable U.S. export laws and regulations.
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# The user has the responsibility to obtain export licenses, or other export
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# authority as may be required before exporting this software to any 'EAR99'
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# embargoed foreign country or citizen of those countries.
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#
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# Authors: Kosal Khun, Marco Lavalle
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#~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~
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# Comment: Adapted from InsarProc/runOrbit2sch.py
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import logging
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import stdproc
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import isceobj
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logger = logging.getLogger('isce.isceProc.runOrbit2sch')
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def runOrbit2sch(self):
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planet = self._isce.planet
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peg = self._isce.peg
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pegHavg = self._isce.averageHeight
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stdWriter = self._stdWriter
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for sceneid in self._isce.selectedScenes:
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for pol in self._isce.selectedPols:
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frame = self._isce.frames[sceneid][pol]
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orbit = self._isce.orbits[sceneid][pol]
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catalog = isceobj.Catalog.createCatalog(self._isce.procDoc.name)
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sid = self._isce.formatname(sceneid, pol)
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orbit, velocity = run(orbit, peg, pegHavg, planet, stdWriter, catalog=catalog, sceneid=sid)
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self._isce.orbits[sceneid][pol] = orbit ##update orbit
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self._isce.pegProcVelocities[sceneid][pol] = velocity ##update velocity
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def run(orbit, peg, pegHavg, planet, stdWriter, catalog=None, sceneid='NO_ID'):
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"""
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Convert orbit to SCH.
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"""
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logger.info("Converting the orbit to SCH coordinates: %s" % sceneid)
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objOrbit2sch = stdproc.createOrbit2sch(averageHeight=pegHavg)
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objOrbit2sch.stdWriter = stdWriter.set_file_tags("orbit2sch",
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"log",
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"err",
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"log")
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objOrbit2sch(planet=planet, orbit=orbit, peg=peg)
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if catalog:
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isceobj.Catalog.recordInputsAndOutputs(catalog, objOrbit2sch,
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"runOrbit2sch." + sceneid,
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logger,
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"runOrbit2sch." + sceneid)
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#Piyush
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####The heights and the velocities need to be updated now.
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(ttt, ppp, vvv, rrr) = objOrbit2sch.orbit._unpackOrbit()
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procVelocity = vvv[len(vvv)//2][0]
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return objOrbit2sch.orbit, procVelocity
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