Ge Aviation Systems Limited

General Electric Company

Terrell Michael Brace

Joachim Karl Ulf Hochwarth

Antonio Lugo Trejo

Víctor Mario Leal Herrera

Troy Stephen Brown

Christian Reynolds Decker

Gregory Reed Sykes

Victor Mario Leal Herrera

Francisco Javier Sanchez Del Valle

Franco Elías Ledesma Orozco

Franco Ledesma Orozco

Francisco Sanchez Del Valle

A system and a method for identifying errors within a modular framework of a system comprising of a flight management system and an error reporting system. The modular components and correlating code modulars of the modular framework can be executed collectively or independently. Each modular component can be designed to incorporate independent modular updates or modifications.

Flight management system and method for reporting an intermitted error

A system for read-access of a regulated system, the system comprising a specialized data store, at least one memory, and a flexible reader. The specialized data store able to receive at least a portion of a set of procedures that define a respective set of systematic data and executable operations. The at least one memory including at least one set of data related to the set of procedures.

Systems and method for flexible write- and read-access of a regulated system

A system and method for flexible writing of internal data of a regulated system can include generating a flexible write instruction, providing the flexible write instruction to the regulated system, and storing or committing data changes to the regulated system outside of the normal system operations, during runtime.

Systems and methods for flexible writing of internal data of regulated system

A system and method for flexible read-access of a set of procedures during runtime of a regulated system, the system comprising a set of procedures each defining a respective set of systematic data and an executable operation, a specialized data store configured to receive at least a subset of procedures, at least one memory including at least one set of data relating to the set of procedures, a receiving component communicatively coupled to the regulated system, and a flexible reader authorized for read-access to the specialized data store and the at least one memory.

Systems and techniques for memory event mitigation in redundant software installations are presented. A system can initiate an event executed by a first software application and a second software application that corresponds to the first software application. First data associated with the first software application can be stored in a first data store and second data associated with the second software application can be stored in a second data store. The system can also compare a first check value for the first data associated with the event and a second check value for the second data associated with the event. Furthermore, the system can re-initiate the event executed by the first software application and the second software application in response to a determination that the first check value does not correspond to the second check value.

Memory event mitigation in redundant software installations

The present disclosure provides systems and methods that enable flexible access of internal data of an avionics system (e.g., a Flight Management System). Aspects of the present disclosure enable enhanced, flexible and robust recording of flight test data, testing, debugging, and analyzing in-service problems. One example system includes a Configuration Tool that generates a Loadable Configuration File and a Configuration File based on user selections, structure of data in Data Stores, platform information, processor information, and Receiving Component requirements; a Data Access Component that subscribes to data in the Data Stores based on the Loadable Configuration File and outputs the data; and a Receiving Component receives the data, and decodes the data based at least in part on the Configuration File. Aspects of the present disclosure provide the ability to change which data gets output by the avionics system without the need to recompile and recertify the avionics system software.

Systems and methods for flexible access of internal data of an avionics system

A method and system for a multi-spectrum celestial navigation system includes a first sensor responsive to at least a first and a second wavelength band of electromagnetic radiation. The sensor is configured to generate a first output related to the first wavelength band of electromagnetic radiation and to generate a second output related to the second wavelength band of electromagnetic radiation. The system also includes a processor programmed to receive the first and second outputs, determine a position of the sensor with respect to one or more stars using a stored star catalog and the received first and second outputs, and output the determined position.

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Ada, MI, United States of America

Terrell Michael Brace