Abstract
This paper presents the modeling and control of an aircraft wing structure constructed by lattice-based cellular materials/components. A novel model reduction process is proposed that utilizes the extended discrete-time transfer matrix method (E-DT-TMM). Through recursive application of the E-DT-TMM, an effective reduced-order model can be obtained in which a decentralized discrete-time linear quadratic regulator (LQR) controller can be designed. To demonstrate the efficiency of the proposed concept, a prototype wing structure is studied. The analysis and simulation results show that the performance of the proposed E-DT-TMM based decentralized LQR controller is comparable with that of the full-state continuous LQR controller.
Original language | British English |
---|---|
Pages (from-to) | 1256-1272 |
Number of pages | 17 |
Journal | Structural Control and Health Monitoring |
Volume | 23 |
Issue number | 10 |
DOIs | |
State | Published - Oct 2016 |
Keywords
- decentralized control
- discrete time
- LQR
- structural control
- transfer matrix method