Integrated flight/propulsion control system design based on a decentralized, hierarchical approach
Integrated flight/propulsion control system design based on a centralized approach
Integrated flight/propulsion control system design based on a centralized approach
Decentralized hierarchical partitioning of centralized integrated controllers
Application of an integrated flight/propulsion control design methodology to a STOVL aircraft
IMPAC - An integrated methodology for propulsion and airframe control
Neural network application to aircraft control system design
Controller partitioning for integrated flight/propulsion control implementation
Piloted Evaluation of an Integrated Methodology for Propulsion and Airframe Control Design
Integrated Flight and Propulsion Controls for Advanced Aircraft Configurations
Aero-Propulsion Control Research in Support of NASA Aeronautics Research Strategic Thrusts