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Created with Raphaël 2.2.021Jan2017161514131098763220Dec191817161312111096543229Nov282726252221201815126Fixed descriptionnew polar calculation methodMerge branch 'fix/aerodynamic_analysis_LILI' into 'develop'aerodynamic_analysis (schueltke): LILI input adaptionFixed plot path and added design point tableMerge branch 'develop' of ssh://git.rwth-aachen.de/unicado/aircraft-design into developMerge branch 'feature/empennage_design_t_tail' into 'develop'[FEATURE] T-TailMerge branch 'documentation/landing_gear_design_update' into 'develop'design_method.md: Updated design methodMerge branch 'feature/mission_analysis_strategy_change' into 'develop'mission_analysis: rebranding strategypropulsive Fuselage extensionAdded design point outputMerge branch 'develop' of ssh://git.rwth-aachen.de/unicado/aircraft-design into developMerge branch 'feature/constraint_analysis_comments' into 'develop'Fixed _conf.xmlreturn to nelder-meadRoll backwardsMerge branch 'feature/update_Create_Mission_XML_naming' into 'develop'Naming and comment updateMerge branch 'feature/aerodynamic_analysis_html_report' into 'develop'aerodynamic_analysis (schueltke): Adaption HTML reportMerge branch 'feature_clean_and_advance' into 'develop'CMakeLists.txt: Added necessary line to include new libadded aircraftsimulationMerge branch 'fix/Cl_distribution_interpolation' into 'develop'revert cl interpolation to previous stateMerge branch 'fix/trimm_problems' into 'develop'custom stabilizer angles for trim are now possibleMerge branch 'fix/wave_drag_calculation' into 'develop'Fixes in Cl interplation from lift distributionadded package files for fmaupdated tester.py for trimroutine -> should work better nowusermethoddatapreparation:small_changesrenamed thrust_share_OEIOEI and MLM fixrun trimroutine with new optimizer -> seems to workfixed missing thrust output on default aerosonde parameters
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