Abstract Systems and methods of prioritizing the use of flight attitude controls of aircraft
operable to transition between thrust-borne lift in a VTOL orientation and wing-borne lift in a …

Techniques to control flight of an aircraft are disclosed. In various embodiments, a set of
inputs associated with a requested set of forces and moments to be applied to the aircraft is …

A system for flight control in electric aircraft includes a flight controller configured to provide
an initial vehicle torque signal including a plurality of attitude commands. The system …

A device and method for flying an aircraft is disclosed. According to one example, the device
includes a vehicle management computer configured to position a plurality of control …

A system for fault detection and control in an electric aircraft including an inertial
measurement unit, the inertial measurement unit including at least a sensor configured to …

A multi-rotor aircraft includes a fuselage, a propulsion engine coupled to the fuselage that
generates thrust to propel the aircraft along a first vector during forward flight, and rotors …

Thrust values for motors in an aircraft are generated where each flight controller in a plurality
of flight controllers generates a thrust value for each motor in a plurality of motors using an …

A geometry-based flight control system is disclosed. In various embodiments, a set of
inceptor inputs associated with a requested set of forces and moments to be applied to the …

US11299289B1 - Angle-of-attack determination for aircraft stall protection - Google Patents
US11299289B1 - Angle-of-attack determination for aircraft stall protection - Google Patents …

Systems and methods for controlling thrust of an engine for an aircraft are described herein.
A position of a thrust lever for controlling the engine is obtained from one or more sensors …