Convert Aircraft.Wing.LOAD_DISTRIBUTION_CONTROL to variable - #1273
Convert Aircraft.Wing.LOAD_DISTRIBUTION_CONTROL to variable#1273xjjiang wants to merge 14 commits into
Conversation
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How much of this issue is addressed by this PR: |
Only bullet number 3 of Issue #911 is addressed. Bullets number 1 and 2 are related (for |
Thanks @xjjiang - I have made a note on the Issue that part 3 has already been done in this PR. |
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I used AI to help create a visualization of the change in intensity methods showing the differences in value, gradient and the smoothed discontinuity in gradient.
load_intensity_smoothing_test.txt I think we could do with some 2nd opinions from @jkirk5 and @Kenneth-T-Moore on this change! |
FLOPS does a simple linear interpolation. It will fail for gradient. I can wait for Jason and Ken. Before we discuss, I will keep function |
…-Aviary into Var_LOAD_DISTRIBUTION_CONTROL

Summary
Option
Aircraft.Wing.LOAD_DISTRIBUTION_CONTROLis converted to an Aviary variable.This is part of issue #598.
Related issue: #911.
Related Issues
Backwards incompatibilities
None
AI Usage
A quartic polynomial interpolation is generated by ChatGPT to get a smooth version of
load_intensity_by_factor(). It interpolates at 1, 1.5, 2, 2.5, and 3.