Open
Milestone
Mar 1, 2025–Nov 30, 2025
Milestone Final v1.0
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Unstarted Issues (open and unassigned)
17
- unicado.gitlab.io · Add user and developer documentation for libraries
- Aircraft Design · Implement new method using calibration based on higher fidelity data
- Aircraft Design · Check reference year correction
- Aircraft Design · Make outputs in dollar
- Aircraft Design · Discuss if the V-n diagram can be included in the constraint_analysis
- Aircraft Design · Check if LTO is already checked and can be skipped
- Aircraft Design · Discuss if initial_sizing and constraint_analysis can be merged into one tool
- Aircraft Design · Discuss if limit equations should be provided as libraries
- Aircraft Design · Include top-of-climb and approach speed limit
- Aircraft Design · Discuss what CLmax is written in the acXML by aerodynamic_analysis
- Aircraft Design · Update config xml
- Aircraft Design · Calculate dive speed for landing_gear_design
- Aircraft Design · Simplify standard mission method by eliminating mission below FL15
- Aircraft Design · Reduce multiple precision settings to one (time increment)
- RCE Workflow · Workflow: change prints in console and log file in post_operation_of_design_sizing
- RCE Workflow · Workflow: Include lower boundary for convergence criteria
- Aircraft Design · empennage_design: include new method resizing acc to stability
Ongoing Issues (open and assigned)
16
- Aircraft References · Discuss necessity of maximum_structrual_payload_mass
- Aircraft Design · aerodynamic_analysis: reactivate adapt polars to cruise Mach number
- Aircraft Design · systems_design: implement a low fidelity method
- unicado.gitlab.io · aerodynamic_analysis: define process how to set up the calibration factors
- Aircraft Design · Aerodynamic_analysis: check high-lift angle of attack
- Aircraft Design · propulsion_design & landing_gear_design: Discuss how to handle interference if pushed to much outboards
- Aircraft Design · landing_gear_design: implement a low fidelity method
- Aircraft Design · landing_gear_design: Adapt maximum achievable CL
- Aircraft Design · propulsion_design & aerodynamic_analysis: shift nacelle drag to net thrust
- RCE Workflow · Workflow: discuss wing tank sizing control
- Aircraft Design · fuselage_design: implement a low fidelity method
- Aircraft Design · initial_sizing: calculate fuel mass with MTOM-OME-PL
- RCE Workflow · Check if check_tlars_and_gradients in RCE is still necessary
- RCE Workflow · Discuss whether constraint analysis should not be executed every iteration
- Aircraft Design · Extract a point_performance_analysis tool from mission_analysis
- RCE Workflow · Enable pep8 for new tools
Completed Issues (closed)
2
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