Abstract: According to certain aspects of the disclosure, a computer-implemented method may be used for detecting health status of an environmental control system. The method may include receiving aircraft data of an aircraft and receiving flight data of an aircraft. Calculating a predicted performance of the aircraft based on the received aircraft data and the received flight data and generating at least one model scalar or residual, wherein the at least one model scalar or residual is generated based on the aircraft data of the aircraft. Identifying at least one pattern from the at least one model scalar or residual and classifying the at least one pattern into at least one of a plurality of classifications. Identifying a failure of modes or components from the classifications and transmitting a maintenance report once the failure of modes or components is identified.

Abstract: Systems and methods are disclosed for providing model-based diagnostics and analytics for wind turbine generators. Methods comprise: obtaining design data of one or more wind turbines, the design data including one or combinations of failure modes and effects analysis, diagrams/schematics for mechanical, electrical, hydraulic, and pneumatic systems, software logic diagrams, Interface Control Diagrams, component failure rates, a net list, fault codes, troubleshooting manuals, and/or component costs; and generating a wind turbine model based on the design data by: generating relationship models based on the FMEAs, the component failure rates, and/or the component costs; generating sub-system models based on the diagrams/schematics for mechanical, electrical, hydraulic, and pneumatic systems, the software logic diagrams, and/or the ICDs; and logically integrating the sub-system models and the relationship models to form the wind turbine model.

Abstract: According to certain aspects of the disclosure, a computer-implemented method may be used for detecting health status of an environmental control system. The method may include receiving aircraft data of an aircraft and receiving flight data of an aircraft. Calculating a predicted performance of the aircraft based on the received aircraft data and the received flight data and generating at least one model scalar or residual, wherein the at least one model scalar or residual is generated based on the aircraft data of the aircraft. Identifying at least one pattern from the at least one model scalar or residual and classifying the at least one pattern into at least one of a plurality of classifications. Identifying a failure of modes or components from the classifications and transmitting a maintenance report once the failure of modes or components is identified.