L1 Adaptive Control for Tilt-Wing VTOL UAV-Reference-Cited by-同舟云学术

L1 Adaptive Control for Tilt-Wing VTOL UAV

Published:2021-12-03 Issue: Volume: Page:
ISSN:
Container-title:2021 International Conference on Mechanical, Aerospace and Automotive Engineering
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Author:

Wang Fengqiu¹,Zeng Yaohua¹,Zeng Tie¹,Lai Yumin¹,Liu Chuanlong¹,Wei Wei¹

Affiliation:

1. System Engineering Institute of Sichuan Aerospace, China

Publisher

ACM

Link

https://dl.acm.org/doi/pdf/10.1145/3518781.3519207

Reference17 articles.

1. Rothhaar P M Murphy P C Bacon B J NASA Langley Distributed Propulsion VTOL Tilt-Wing Aircraft Testing Modeling Simulation Control and Flight Test Development[J]. 2014 Rothhaar P M Murphy P C Bacon B J NASA Langley Distributed Propulsion VTOL Tilt-Wing Aircraft Testing Modeling Simulation Control and Flight Test Development[J]. 2014

2. William J Mark A Zachary R. NASA GL-10 Tilt-Wing VTOL UAS Flight Validation Experiments[J]. 2015 William J Mark A Zachary R. NASA GL-10 Tilt-Wing VTOL UAS Flight Validation Experiments[J]. 2015

3. Padhi R Rakesh P. Formation Flying of UAVs with Dynamic Inversion Based Partial Integrated Guidance and Control[C]. 2013 Padhi R Rakesh P. Formation Flying of UAVs with Dynamic Inversion Based Partial Integrated Guidance and Control[C]. 2013

4. Miller C. Nonlinear Dynamic Inversion Baseline Control Law: Architecture and Performance Predictions[C]. 2011 Miller C. Nonlinear Dynamic Inversion Baseline Control Law: Architecture and Performance Predictions[C]. 2011

5. Cao C , Hovakimyan N. Design and Analysis of a Novel L1 Adaptive Controller, Part I: Control Signal and Asymptotic Stability[C] . IEEE , 2006 Cao C, Hovakimyan N. Design and Analysis of a Novel L1 Adaptive Controller, Part I: Control Signal and Asymptotic Stability[C]. IEEE,2006