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Created with Raphaël 2.2.017Jan161514131098763220Dec191817161312111096543229Nov282726252221201815126aerodynamic_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 parametersFixed Build-ErrorsMerge branch 'feature/fuslage_design' into 'develop'Feature/fuslage designAanother small cleanupSmall cleanupFixed issuesMerge branch 'fix/systems_design_delta_ISA' into 'develop'Fix use of delta_ISA in systems_designintermediate saveMerge branch 'fix/aerodynamic_analysis' into 'develop'Make aero analysis buildableDid some cleaning and tried to make stuff more readableMade some changes for html outputfeature/tank_de…feature/tank_design_liquid_hydrogenIncrease readabilityMerge branch 'feature/aero_html_report' into 'develop'Add aerodynamic_analysis html reportMerge branch 'feature/landing_gear_design_html_report' into 'develop'landing_gear_design: Add HTML report functionMerge branch 'feature/fuselage_design_add_html_output' into 'develop'fuselage_design: Add HTML report functionMerge branch 'feature_one_more_command_output' into 'develop'deletes stupid comment