landing_gear_design: - fix minimum percentage of nose gear load error for...

Description

• Add if and else condition to set the minimum and maximum percentage of nose gear load depending on the aircraft configuration.
• Add option to set specific values for the minimum and maximum percentage of nose gear load in the module configuration file

Related Issue(s)

• no related issues

Other Changes

• no other changes

Screenshots/Logs

Attach screenshots or log outputs if applicable.

Testing Instructions

1. [Step 1: Copy python code and configuration file of landing gear design to your local UNICADO installation]
2. [Step 2: Run the workflow for different aircraft types (single_aisle, wide_body, tube_and_wing, blended_wing_body, LH2)]
3. [Step 3: check if landing gear occurs an error or not]

Developer Checklist

• Code has been tested locally and/or in pipeline.
• (if applicable) documentation updated.
• (if applicable) impact of new dependencies reviewed and included in project.
• Merge conflicts resolved with the target branch.

Additional Notes

tested locally by @AndiGob for different aircraft configurations -> no errors occurred.

changed milestone to %Beta v0.6.0

added modulelanding_gear_design typefeature labels

requested review from @Florian.Schueltke and @philipp.hansmann

assigned to @tobi747

added 1 commit

• 33cd5e75 - landing_gear_design: - fix to skipp nacelle ground clearance check if no...

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added 1 commit

• 872fead1 - landing_gear_design: - update description of module configuration file...

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Accepted from code style view. @philipp.hansmann: Please check execution for blended_wing_body configuration

approved this merge request

approved this merge request

mentioned in commit 9d04b9df

merged