Research on Lateral-Directional Dynamic Characteristics and Control for Large Envelope Flight of Modular Aircraft

DOI

10.2991/mme-16.2017.1How to use a DOI?

Keywords

Modular aircraft, Large envelope flight, Lpv, Dynamic characteristics, Self-scheduled parameter adjustment.

Abstract

The linear parameter varying (LPV) system model of the lateral-directional dynamics for large envelope flight of modular aircraft including various configurations was built. The validity of the aircraft LPV model was verified by the comparison of dynamic simulation between the LPV model and the nonlinear model. The lateral-directional dynamic characteristics under different configurations of modular aircraft in large flight envelope were studied. The stability augmentation system (SAS) for the inner loop and the self-scheduled parameter adjusting H robust controller for the outer loop of the control system were designed based on the lateral-directional dynamic LPV model of modular aircraft to guarantee the control effect for aircraft lateral-directional motion. The closed loop system was simulated and the simulation results indicate the integrated control system could achieve precision tracking of modular aircraft lateral-directional command signals under different configurations in large flight envelope.

Copyright

© 2017, the Authors. Published by Atlantis Press.

Open Access

This is an open access article distributed under the CC BY-NC license (http://creativecommons.org/licenses/by-nc/4.0/).

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TY  - CONF
AU  - Wen-Xin Zhang
AU  - Li-Xin Wang
AU  - Ting Yue
PY  - 2016/12
DA  - 2016/12
TI  - Research on Lateral-Directional Dynamic Characteristics and Control for Large Envelope Flight of Modular Aircraft
BT  - Proceedings of the 3rd Annual International Conference on Mechanics and Mechanical Engineering (MME 2016)
PB  - Atlantis Press
SP  - 1
EP  - 11
SN  - 2352-5401
UR  - https://doi.org/10.2991/mme-16.2017.1
DO  - 10.2991/mme-16.2017.1
ID  - Zhang2016/12
ER  -