Decentralized hierarchical partitioning of centralized integrated controllersA framework for a decentralized hierarchical controller partitioning structure is developed. This structure allows for the design of separate airframe and propulsion controllers which, when assembled, will meet the overall design criterion for the integrated airframe/propulsion system. An algorithm based on parameter optimization of the state-space representation for the subsystem controllers is described. The algorithm is currently being applied to an integrated flight propulsion control design example.
Document ID
19920046495
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Schmidt, Phillip (Akron, University OH, United States)
Garg, Sanjay (NASA Lewis Research Center Cleveland, OH, United States)