Attendance
Sysint
Mech
Working on a calculator that outputs range, speed based on input airfoils
Nose separate from frame, will mount to fuselage to experiment with different nose shapes
One tube between fuselage and tail (aluminum)
Airfoil selection is done (NACA 4412), frame design is in progress
EE
BMS for the fixed wing by end of fall term
6S servo module not started yet, hoping for design by end of term
EFS
Parts of zeropilot are not compiling, investigating
CAN to dshot converter is coming along well, aim to use around first flight of fixed wing