A 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.
Decentralized hierarchical partitioning of centralized integrated controllers
1991 American Control Conference ; 1991 ; Boston, MA, United States
1991-01-01
Conference paper
No indication
English
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