Main differences between V7.2 and V7.2.1
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Non obfuscated methods
- the LEOManIncInfo.getInc() method is now available (no more obfuscated)
Additional output information
- Adding the margin on the reentry date as below:
Re-entry date : 2011-11-30T15:37:29.221 Re-entry date error : 0.106 (days)
- When Orbit Determination (OD) is not successful, reentry date (and margin on it) using the refined S/m is still displayed
- adding units on S/m results:
SmDragApriori : 0.05916134793505359 kg/m2 SmDragRefined : 0.05457889062590913 kg/m2 SmDragAfterOD : 0.050351376463313384 kg/m2 SmSRPRefined : 0.0 kg/m2
- Changing type of font for better readibility.
Anomaly corrections
- When the computation exits in error mode due to the OperaException type (typically if there is a problem when reading TLE), the management of such exception allows now going on computation for next Norad Ids.
- OPERA does correctly take into account PATRIUS_DATASET and the Opera configuration file for some batch configurations (for Search by Sat or Search by Orb options).
- The Opera configuration file (including all the by default configurations) is now correctly read if the name of a directory will start by "/".
- No more erroneous error messages between BYSAT et BYORB.