A Near-Hover Adaptive Attitude Control Strategy of a Ducted Fan Micro Aerial Vehicle with Actuator Dynamics

Applied Sciences ◽

10.3390/app5040666 ◽

2015 ◽

Vol 5 (4) ◽

pp. 666-681 ◽

Author(s):

Shouzhao Sheng ◽

Chenwu Sun

Keyword(s):

Control Strategy ◽

Attitude Control ◽

Micro Aerial Vehicle ◽

Actuator Dynamics ◽

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Modeling and attitude control analysis of a ducted-fan micro aerial vehicle

Control Engineering Practice ◽

10.1016/j.conengprac.2009.09.009 ◽

2010 ◽

Vol 18 (3) ◽

pp. 209-218 ◽

Author(s):

J.-M. Pflimlin ◽

P. Binetti ◽

P. Souères ◽

T. Hamel ◽

D. Trouchet

Keyword(s):

Attitude Control ◽

Control Analysis ◽

Micro Aerial Vehicle ◽

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Pendulum-like oscillation controller for micro aerial vehicle with ducted fan based on LQR and PSO

Science China Technological Sciences ◽

10.1007/s11431-012-5065-5 ◽

2012 ◽

Vol 56 (2) ◽

pp. 423-429 ◽

Author(s):

HaiBin Duan ◽

ChangHao Sun

Keyword(s):

Micro Aerial Vehicle ◽

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On Position and Attitude Control of Flapping Wing Micro-aerial Vehicle

Advances in Neural Networks – ISNN 2020 - Lecture Notes in Computer Science ◽

10.1007/978-3-030-64221-1_18 ◽

2020 ◽

pp. 207-216

Author(s):

Dexiu Ma ◽

Long Jin ◽

Dongyang Fu ◽

Xiuchun Xiao ◽

Mei Liu

Keyword(s):

Attitude Control ◽

Flapping Wing ◽

Micro Aerial Vehicle ◽

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Experimental and Theoretical Study of Attitude Control of Flapping Wing Micro Aerial Vehicle

41st AIAA Fluid Dynamics Conference and Exhibit ◽

10.2514/6.2011-3253 ◽

2011 ◽

Author(s):

Koji Isogai ◽

Hiroyasu Kawabe ◽

Hiroto Nagai ◽

Shun Nishiguchi

Keyword(s):

Attitude Control ◽

Theoretical Study ◽

Flapping Wing ◽

Micro Aerial Vehicle ◽

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Dynamic modeling using system identification and attitude control design of GaneFly flapping wings micro aerial vehicle (FWMAV)

2017 7th IEEE International Conference on System Engineering and Technology (ICSET) ◽

10.1109/icsengt.2017.8123446 ◽

2017 ◽

Author(s):

R. S. Brian Benyamin ◽

Muhammad Aldo Aditiya Nugroho ◽

A. Yosua Sepri ◽

Bambang Riyanto Trilaksono ◽

Agoes Moelyadi

Keyword(s):

System Identification ◽

Dynamic Modeling ◽

Attitude Control ◽

Control Design ◽

Flapping Wings ◽

Micro Aerial Vehicle ◽

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Attitude Control of Flapping Wing Micro Aerial Vehicle Based on Double Fuzzy Sliding Mode Control

Advanced Materials Research ◽

10.4028/www.scientific.net/amr.468-471.704 ◽

2012 ◽

Vol 468-471 ◽

pp. 704-707

Author(s):

Sheng Bin Hu ◽

Wen Hua Lu ◽

Zhi Yi Chen ◽

Lei Lei ◽

Yi Xuan Zhang

Keyword(s):

Sliding Mode Control ◽

Attitude Control ◽

Fuzzy Controller ◽

Sliding Mode ◽

Micro Aerial Vehicle ◽

Fuzzy Sliding Mode Control ◽

Mode Control ◽

Control Scheme ◽

Aerial Vehicle ◽

Fuzzy Sliding Mode

An adaptive Double Fuzzy Sliding Mode Control scheme for attitude control of Flapping Wing Micro Aerial Vehicle is proposed in this paper. Based on the feedback linearization technique, a sliding mode controller is designed. To faster response speed, a fuzzy controller is designed to adaptively tune the slope of sliding mode surface. To reduce the chattering, another fuzzy controller is designed to adaptively tune the switch part of sliding mode control. The system stability is proved by Lyapunov principle. Simulation results show that the proposed control scheme is effective.

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Bounded attitude control of a Flapping wing Micro Aerial Vehicle using direct sensors measurements

2009 IEEE International Conference on Robotics and Automation ◽

10.1109/robot.2009.5152713 ◽

2009 ◽

Author(s):

H. Rifai ◽

J.-F. Guerrero-Castellanos ◽

N. Marchand ◽

G. Poulin

Keyword(s):

Attitude Control ◽

Flapping Wing ◽

Micro Aerial Vehicle ◽

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Robust attitude control design for a low-cost hexarotor micro aerial vehicle

Transactions of the Institute of Measurement and Control ◽

10.1177/0142331215625768 ◽

2016 ◽

Vol 38 (6) ◽

pp. 701-721 ◽

Author(s):

Dafizal Derawi ◽

Nurul Dayana Salim ◽

Hairi Zamzuri ◽

Mohd Azizi Abdul Rahman ◽

Kenzo Nonami

Keyword(s):

Attitude Control ◽

Low Cost ◽

Control Design ◽

Micro Aerial Vehicle ◽

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Modelling and attitude control of novel multi-ducted-fan aerial vehicle in forward flight

International Journal of Modelling Identification and Control ◽

10.1504/ijmic.2019.10017478 ◽

2019 ◽

Vol 31 (1) ◽

pp. 81

Author(s):

Lu Lin ◽

Wanming Chen ◽

Yue Ma

Keyword(s):

Attitude Control ◽

Forward Flight ◽

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Attitude Control of Flapping-wing Micro Aerial Vehicle Based on Active Disturbance Rejection Control

2011 International Conference on Internet Computing and Information Services ◽

10.1109/icicis.2011.103 ◽

2011 ◽

Author(s):

Hongjun Duan ◽

Qingwei Li

Keyword(s):

Attitude Control ◽

Disturbance Rejection ◽

Flapping Wing ◽

Active Disturbance Rejection Control ◽

Micro Aerial Vehicle ◽

Active Disturbance Rejection ◽

Disturbance Rejection Control ◽

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