Hi all,
I'm currently using the battery ducted fan network in SUAVE to investigate an aircraft that uses that type of propulsion system and have successfully got it all implemented, alongside a complete mission analysis (much like the one from the Boeing 737 tutorial).
What I would like to do now though is incorporate the "plot_battery_pack_conditions" function into my mission plots so that I can see how the battery has performed during the mission, much like the outputs of the eVTOL tutorial.
I've had a look and initially the request for that plot type flagged an error that:
"'Conditions' object has no attribute 'battery_current'",
which I believe was because the assignment within the battery ducted fan network was under "'conditions.propulsion.current'" and not "'conditions.propulsion.battery_current'".
Having changed that, it quickly became apparent though that the issues extended beyond that in the sense that whilst in the Lift_Cruise.py network used in the eVTOL tutorial has a substantial amount of code within it dedicated to feeding back battery conditions and states during segments, that these did not feature in the Battery_Ducted_Fan.py network.
I had a go myself at trying to work out what would be needed in the Battery_Ducted_Fan.py network in order to achieve this, but as I'm still fairly new to Python and SUAVE (although getting better each day!), I did get a bit lost.
I know that the SUAVE team are very busy with a multitude of different things, but if anyone had some potential advice as to where to look in particular or pointers to the key features that would need to carry over from the Lift_Cruise.py network into the Battery_Ducted_Fan.py network, it would very much be appreciated!
Hope everyone has a great weekend!
Kind regards,
Jon