Version 4.16 (C, C++, Java Libraries) of the Earth Observation Mission CFI Software (v4.X branch) has been released and can be downloaded here.

Release Notes are available here.

User registration is required. Please find detailed instructions here.

The following is a summary of new features and problems solved:

  • New functionality to calculate Area of Interest based on SDF and time interval
  • Added support for field of view definition of Sun/Moon looking instrument
  • New functionality to perform orbit data check/validation (w.r.t. to configurable thresholds)
  • Added user-friendly definition (enums) of attitude model parameters  
  • Enabled support for ACE2 DEM 5arcmin
  • Enabled support of TLE for Sentinel-5P, Sentinel-3B and Aelous
  • 725 - Corrected the calculation of the Mean Local Solar Time drift
  • 734 - Adjusted limitation of number of characters in input paths to accept path lengths up to the limit imposed by the Linux kernel
  • 735 - Enabled deterministic resource in the Java API by making Attitude and Target implement AutoCloseable
  • 741 - Corrected the configuration of MetopSG attitude using Attitude Definition File (ATTDEF)
  • 746 - Enabled handling void values in DEM (warning when geolocating using void values; indirect use of void values reported as error)
  • 757 - Corrected issue in schema validation of DEM configuration files

 

The openSF Roadmap covering the upcoming releases (3.7.3, 3.7.4, 3.7.5) has been updated and can be accessed from here

Version 4.15 (C, C++, Java Libraries) of the Earth Observation Mission CFI Software (v4.X branch) has been released and can be downloaded here.

Release Notes are available here.

User registration is required. Please find detailed instructions here.

The following is a short list of new features and problems solved:

  • 716 Updated EOCFI system requirement (gcc 6.3, Visual studio, OSX Sierra)
  • 649 - Generation of Restituted Orbit File from TLE file is not allowed in combination with time file
  • 711 - xd_xml_validate: Segmentation fault when schema is given as an absolute path in the file header
  • 712 - xp_get_attitude_data does not raise an error if the nominal attitude is not initialised
  • 727 - xl_time_processing_to_ascii: Internal Error: "Output ascii day is out of range"
  • 730 - targetListInter: outliers with ACE2 DEM

Version 4.14 (C, C++, Java Libraries) of the Earth Observation Mission CFI Software (v4.X branch) has been released and can be downloaded here.

Release Notes are available here.

User registration is required. Please find detailed instructions here.

 

The following is a short list of new features and problems solved:

New Features

  • Support for new mission: FLEX
  • Tools and functions for generation of orbit and attitude file: TLE file is allowed as input
  • Orbit propagation (e.g. xo_osv_compute function): when the orbit Id is initialised with a TLE file it is allowed to propagate after 1 day of the TLE epoch
  • Visibility library, xv_zonevistime_compute function: visibility segments can be calculated also with a ROF (Restituded Orbit File) covering less than one orbit
  • Visibility functions: visibility segments can be computed with a new instrument swath geometry defined by azimuth and incidence angle
  • The Swath Definition File format has been extended to support a new geometry type: Incidence angle
  • New attitude model: MetOp-SG
  • New functions to convert CCSDS Unsegmented Time Code (CUC) to processing time (and vice-versa)
  • Support for Jason-CS Doris files
  • Function xv_gen_scf (Visibility library) generates SCF files compliant with ESOV supported format
  • New function xp_free_target_id_data (Pointing library) to release data of xp_target_id_data type

Major problems solved

  • 656 - Zone visibility function does not calculate all segments when using TLE file (Problem reported by the ESOV development team)
  • 684 - ANX MLST calculated by the xo_orbit_info is not correct when an Orbit Scenario File with MLST drift different from zero is used
  • 703 - targetListInter crash when no Intersection between LOS vector and Earth Surface (Problem reported by the EPS-SG INR team (EUMETSAT))
  • 704 - xo_orbit_init_def: wrong validity time (Problem reported by the ESOV development team)
  • 708 - targetListInter: exception when no solution is found

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