New Release Announcement - OSFI v3.5.5
OSFI v3.5.5 has been released and can be downloaded here.
Changes
- Enabled the use of `E2E_HOME` as base directory for FILE/FOLDER relative paths
- Enabled empty rows and layers in ARRAY parameters
- Added Dockerfiles for supported OSFI build environments -- Linux and Windows
- The values of TIME parameters are now be comparable (total ordering)
- Unit tests introduced to the C and Fortran APIs
- Improved const correctness of C API
Release Notes are available here.
New Release Announcement - EOCFI v4.19
Earth Observation Mission CFI Software v4.19 has been released!
The latest version can be downloaded here with the detailed release notes available here.
User registration is required. Please find detailed instructions here.
The following is a summary of new features and problems solved in Version 4.19.
New Features & Improvements
- Enabled support for ASTER Global Digital Elevation (GDEM) V3
- Enabled orbit initialization based on CCSDS OEM XML files
- Enabled support for <Reference_Frame> tag in Attitude Angles files
- Defined size of file paths based on X*_MAX_PATH macro
- Corrected setSilent()/setVerbose() for EOCFI C++ libraries
- Enabled using repeat cycle of 1 day in OSF
- Improvements to the Software User Manual
Bug Fixes
- Extended xv_orbit_extra to allow calculating results up to 2050
- Corrected xp_sat_nominal_att_init_file to handle star tracker attitude files
- Corrected xp_instr_att_init_file to handle star tracker attitude files
- Adjusted internal threshold to allow calculate Aeolus nominal attitude reference frame in xp_attitude_compute
- Enabled passing NULL as unused time1/time0 and orbit0/orbit1 parameters in xl_time_ref_init_file and xo_orbit_init_file
- Corrected memory leak in xl_change_cart_cs when converting from XL_BM1950 to XL_BM2000
Update: E2E Performance Simulator Generic Requirements Template
Version 1.3 of the "Generic E2E Performance Simulator and L1PP/L2PP Requirement Document " has been published and can be downloaded from here.
It includes major updates and clarifications, restructuring of requirements for L1 and L2 Processor Prototypes, recommendations on the GSM-ISM interface and inputs for SoW.
New Release Announcement - S2G v2.4.5
Version 2.4.5 of the S2G Data Viewer has been released and can be downloaded here.
Release Notes are available here.
User registration is required. Please find detailed instructions here.
New Features
- Update to Eclipse RCP 4.8 (Photon) SDK using compatibility layer
- New splash-screen
Corrections
- ANR-197: Performance decrease observed during TF to ISP transformation
- ANR-223: Sequence Source Counter gaps error wrongly reported for ISPs with different APIDs
- ANR-228: Plot not correct if the path to the field given as X or Y axis does not exist for a given data unit
- ANR-230: Split by APID did not work during TF to ISP transformation and the first TF was skipped
New Mission Schemas
- MetOp-SG-A Ka-band
- MetOp-SG-B Ka-band
- Sentinel-4 X-band
Updated Mission Schemas
- EarthCARE X-band
- Sentinel-5 X-band
- Sentinel-6 X-band
- Seosat X-band
New Release Announcement - SAMIEdit v1.3.5.2
Version 1.3.5.2 of SAMIEdit (SAtellite MIssions 3D visualisation application) has been released and can be downloaded here.
Release Notes are available here.
User registration is required. Please find detailed instructions here.
New Features
- Integration of the following new satellite model with example mission files:
- SEOSAT
- Updates on the following existing satellite models:
- EarthCARE
- Sentinel-6
- Time block improvements (add multiple blocks with given repetition pattern, clear timeline)
- Config.xml: Added customisation of satellite / ground station billboard colours and sizes, satellite model average brightness, default folder for exported images/movies, camera mode at start-up
- Enable/disable display of direction from satellite to the Moon
- Animation triggered through contextual met (right-click) on 3D satellite part
- Up-to-date mission configuration files and example projects
Bug Fixes
- Text overlay info (seconds since ANX, orbit number) does not handle properly leading zeroes
- Reset of history tracks produces graphical artefacts under certain circumstances
- Drop-down menu items present a spurious disabled state under certain circumstances
- The creation //edition of satellite thrusters timeline behaves incorrectly
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