Deterministic Quadrotor static pitch trim T_front/T_rear = (L_half + x_cg)/(L_half - x_cg) + shrouded rotor tip-gap efficiency & vortex-ring descent velocity boundary engine (.json, .csv, .pdf) built for GEPRC CineLog, iFlight Protek, DJI Avata / O3, T-Motor — zero-upload ephemeral Wasm RAM execution.
Running ephemeral Wasm verification…