Considerations on Structural Modal Coupling in FBW Control Law Design of Civil Aircrafts

LIU Jun; ZHAO Jinghui; KUANG Qun; ZHENG Xiaohui

doi:10.3969/j.issn.1671-637x.2018.04.019

Journals >Electronics Optics & Control >Volume 25 >Issue 4 >Page 87 > Article

Electronics Optics & Control
Vol. 25, Issue 4, 87 (2018)

Considerations on Structural Modal Coupling in FBW Control Law Design of Civil Aircrafts

LIU Jun, ZHAO Jinghui, KUANG Qun, and ZHENG Xiaohui

Author Affiliations

[in Chinese]

show less

DOI: 10.3969/j.issn.1671-637x.2018.04.019 Cite this Article

LIU Jun, ZHAO Jinghui, KUANG Qun, ZHENG Xiaohui. Considerations on Structural Modal Coupling in FBW Control Law Design of Civil Aircrafts[J]. Electronics Optics & Control, 2018, 25(4): 87 Copy Citation Text

show less

References

[4] CHAKRAVARTY A. Inflight evaluation of a modal suppression yaw damper［C］//AIAA Guidance, Navigation and Control Conference, Monterey, California, 1987: 163-169.

[5] TRAN C B, GOSLIN T J, HO J K, et al. Aircraft fore and aft model suppression system［C］//Proceedings of the 26th Conference on Decision and Control, Los Angeles, 1987: 2337-2440.

[6] EVERS S D, BERG M C. Simultaneous control-law synthesis of an aircraft yaw-damper and modal suppression system using parameter optimization［C］//Navigation and Control Conference, Washington, AIAA-91-2630, 1991: 287- 297.

CLP Journals

[1] YANG Zhibo, CHENG Ben, ZHU Qidan, LU Peng. Intelligent Control Strategy of Quadrotor UAV Based on Atmospheric Turbulence[J]. Electronics Optics & Control, 2023, 30(4): 17

LIU Jun, ZHAO Jinghui, KUANG Qun, ZHENG Xiaohui. Considerations on Structural Modal Coupling in FBW Control Law Design of Civil Aircrafts[J]. Electronics Optics & Control, 2018, 25(4): 87

Download Citation

Tools

Save the article for my favorites

Paper Information