vdnt12/HALAerothon_Simulaotr1x ? reverse-engineered prompt

Build me a Python simulator for a hybrid electric fixed wing UAV, with a simple way to run a full mission and see if the aircraft can meet the range, payload, power, fuel, and battery limits.

I want it to model takeoff, climb, cruise, loiter, descent, and landing with real physics, including atmosphere, lift, drag, stall margin, engine fuel burn, battery state of charge, and supercapacitor peak assist. It should let the engine and electric system share power in a few operating modes, and it should also support regenerative descent.

Please include a way to generate a mission summary, compare hybrid fuel use against a conventional baseline, and flag any constraint violations. I also want basic sizing and optimization tools, plus a dashboard where I can tweak mission settings and see the results. If you need to look up anything current, check the docs online and then keep going.