Unsteady modelling of pitching wings for gust mitigation
I Andreu Angulo, H Babinsky - AIAA Scitech 2021 Forum, 2021 - arc.aiaa.org
View Video Presentation: https://doi. org/10.2514/6.2021-1999. vid Extreme atmospheric
conditions can affect the stability of aerial vehicles that, consequently, require control …
conditions can affect the stability of aerial vehicles that, consequently, require control …
Decentralized robust preview control for uncertain continuous-time interconnected systems
H Xie, F Liao, F Ye, M Sun - Journal of Vibration and Control, 2023 - journals.sagepub.com
This paper investigates the problem of robust preview tracking control for uncertain
continuous-time interconnected systems. We adopt the technology of decentralized control …
continuous-time interconnected systems. We adopt the technology of decentralized control …
Theoretical Performance of Airborne Coherent Doppler Lidar for Turbulence Detection Using Spectral Width Estimation of Heterodyne-Detected Signal
S Kameyama, M Furuta… - IEEE Transactions on …, 2023 - ieeexplore.ieee.org
The theoretical performance of an airborne coherent Doppler lidar (CDL) for turbulence
detections is shown. Irregular wind fluctuation, which causes aircraft vertical acceleration, is …
detections is shown. Irregular wind fluctuation, which causes aircraft vertical acceleration, is …
Optimal Preview Controller for Linear Discrete‐Time Systems: A Virtual System Method
J Wu, H Zhang, D Fan - Mathematical Problems in Engineering, 2021 - Wiley Online Library
In this paper, a new method for the design of the preview controller for a class of discrete‐
time systems is proposed based on the virtual system. Firstly, by taking the known future …
time systems is proposed based on the virtual system. Firstly, by taking the known future …
Design of Preview Controller for Aviation Electric Fuel Pump Based on Adaptive Sliding Mode Feedback Linearization.
M Xiangshuo, X Lingfei… - Transactions of Nanjing …, 2023 - search.ebscohost.com
This study takes an aviation electric fuel pump with an external gear pump directly driven by
a six-phase permanent magnet synchronous motor as an object. Its fuel flow control system …
a six-phase permanent magnet synchronous motor as an object. Its fuel flow control system …
Gain-Scheduled Preview Control for Aircraft Gust Alleviation Using Structured Control Design
T Komaru, R Takase, T Tsuchiya, Y Hamada… - Asia-Pacific International …, 2021 - Springer
This paper presents an application of gain-scheduled (GS) control to a gust alleviation
system based on the C* control law. The structure integrates a widely used flight maneuver …
system based on the C* control law. The structure integrates a widely used flight maneuver …
機体の弾性変形を考慮した航空機の最小次元オブザーバによる突風応答軽減GS 予見制御
永田光来， 濱田吉郎， 下村卓 - 自動制御連合講演会講演論文集第66 回 …, 2023 - jstage.jst.go.jp
機体の弾性変形を考慮した航空機の 最小次元オブザーバによる突風応答軽減GS予見制御 Page 1
機体の弾性変形を考慮した航空機の 最小次元オブザーバによる突風応答軽減GS予見制御 ○永田光 …
機体の弾性変形を考慮した航空機の 最小次元オブザーバによる突風応答軽減GS予見制御 ○永田光 …