An Application of Optimal Control Theory to the FFG-7 Gas Turbine Propulsion System.
Abstract
An optimal integral control design program was applied to a linearized state variable model of the FFG-7 ship class gas turbine and Controllable Reversible Pitch (CRP) propeller main propulsion system. Various combinations of output parameters were investigated in an attempt to produce a feasible control design. Only one acceptable design was achieved which did not violate any physical constraints. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Jun 01, 1979
- Accession Number
- ADA073870
Entities
People
- Richard A. Kalyn
Organizations
- Naval Postgraduate School