Static flow characteristics of a mass flow injecting valve

Duane Mattern

A comparison of two multi-variable integrator windup protection schemes

Duane Mattern

Integrated flight/propulsion control system design based on a decentralized, hierarchical approach

Duane Mattern

A linear control design structure to maintain loop properties during limit operation in a multi-nozzle turbofan engine

Duane L. Mattern

A comparison of two multi-variable integrator windup protection schemes

Duane L. Mattern

Static flow characteristics of a mass flow injecting valve

Duane L. Mattern

Using neural networks for sensor validation

Autor desconhecido

Comparisons of rig and engine dynamic events in the compressor of an axi-centrifugal turboshaft engine

A. Karl Owen

Application of an integrated flight/propulsion control design methodology to a STOVL aircraft

Sanjay Garg

Application of an integrated methodology for propulsion and airframe control design to a STOVL aircraft

Sanjay Garg

Integrated flight/propulsion control system design based on a centralized approach

Sanjay Garg