This paper presents a modeling and control of aerostructure developed by lattice-based cellular materials/components. The proposed aerostructure concept leverages a building block strategy for lattice-based components which provide great adaptability to varying ight scenarios, the needs of which are essential for in- ight wing shaping control. A decentralized structural control design is proposed that utilizes discrete-time lumped mass transfer matrix method (DT-LM-TMM). The objective is to develop an e ective reduced order model through DT-LM-TMM that can be used to design a decentralized controller for the structural control of a wing. The proposed approach developed in this paper shows that, as far as the performance of overall structural system is concerned, the reduced order model can be as e ective as the full order model in designing an optimal stabilizing controller.
Application of Transfer Matrix Approach to Modeling and Decentralized Control of Lattice-Based Structures
2015 AIAA SciTech Conference ; 2015 ; Kissimmee, FL, United States
2015-01-05
Aufsatz (Konferenz)
Keine Angabe
Englisch
British Library Conference Proceedings | 2015
|Decentralized Variable-Structure Control and its Application to Flexible Structures
British Library Conference Proceedings | 1997
|Decentralized variable-structure control and its application to flexible structures
Online Contents | 1996
|