Aerial vehicle having non-standard priority control and blank-to-yaw control architecture

Abstract

Disclosed implementations describe systems and methods for stabilizing vertical takeoff and landing ('VTOL') or hover flight of a degraded canted-hex aerial vehicle so that the degraded canted-hex aerial vehicle can safely navigate to a landing area. For example, upon detection of a motor-out event, the disclosed implementations may cause an opposing propulsion mechanism of the aerial vehicle to terminate operation, the prioritization of the flight controller to change, and for a feedback loop of the flight controller to provide a preferred thrust to counteract yaw torques acting on the canted-hex aerial vehicle.