The notion of partitioning a centralized controller into a decentralized, hierarchical structure suitable for integrated flight/propulsion control (IFPC) implementation is discussed. A systematic procedure is developed for determining partitioned airframe and engine subsystem controllers (subcontrollers), with the desired interconnection structure, that approximate the closed-loop performance and robustness characteristics of a given centralized controller. The procedure is demonstrated by application to IFPC design for a Short Take-Off and Vertical Landing (STOVL) aircraft in the landing approach to hover transition flight phase.
Controller Partitioning for Integrated Flight/Propulsion Control Implementation
1993
28 pages
Report
No indication
English
British Library Conference Proceedings | 1993
|Integrated Flight and Propulsion Control System Design, via H^ Loop Shaping and Partitioning
British Library Conference Proceedings | 1998
|Total Energy Control System for Helicopter Flight-Propulsion Integrated Controller Design
Online Contents | 2007
|