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Fix problem with scaling up wing area; debug wing AR constraint #133
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At AL=2.0, phi=120: Rpow=0.06e3 => Rpow=0.07e3 =>
with freq limit
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Is the problem due to it choosing min force and in the last one the uinf is dominated by inertial terms? |
Problem with the minlift constraint. Even if AR is similar, the calculated lift is far above the actual lift. If the constraint is being satisfied, how could this happen? |
At least the scaled velocities now make sense. Next check: Faero before vs. Faero next vs. scaled Faero before.
Scaling the red lift by the lift approx function yields this. Should have matched up; but perhaps the error is due to delta y making kinematics worse. |
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Good solution at 300 minal This FD approaches the capability of the BigBee actuator for #131 so will stop here for now. |
Re-running scaling1. Not yet changing Rpow |
Force, power plots are great (solves #128). Freq also good.
-> This was essentially a "fixed wing size" plot |
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…t seems to jump between very high poewr or very low power
Trying to add weight to uinf and Rpow separately
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For scaling1, trying to choose Rpow s.t. for high lift, high stroke, it will choose a high freq |
Unfortunately it seems to never pick high power with u2 norm. Need uinfnorm back to get that flexibility again. |
Bad results |
Closes #128
Related to #131