2015
DOI: 10.1007/978-3-319-18914-7_47
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Robust Linear Longitudinal Feedback Control of a Flapping Wing Micro Air Vehicle

Abstract: Abstract. This paper falls under the idea of introducing biomimetic miniature air vehicles in ambient assisted living and home health applications. The concepts of active disturbance rejection control and flatness based control are used in this paper for the trajectory tracking tasks in the flapping-wing miniature air vehicle (FWMAV) time-averaged model. The generalized proportional integral (GPI) observers are used to obtain accurate estimations of the flat output associated phase variables and of the time-va… Show more

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Cited by 2 publications
(2 citation statements)
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“…• Control Algorithm: It is used to calculate what inputs should be applied to the quadrotor model in order to follow a specific trajectory reference, thereby ensuring that the UAV is correctly positioned and oriented during the monitoring flight. For this component, we designed a generalised proportional integral (GPI) controller based on the flatness theory that demonstrated good results in both stabilisation and tracking tasks, even in the presence of atmospheric disturbances and noise measurements, improving the performance of a traditional PID controller [16][17][18][19][20][21][22][23]. The theoretical details of the GPI control scheme are described in [15].…”
Section: Uav Simulatormentioning
confidence: 99%
“…• Control Algorithm: It is used to calculate what inputs should be applied to the quadrotor model in order to follow a specific trajectory reference, thereby ensuring that the UAV is correctly positioned and oriented during the monitoring flight. For this component, we designed a generalised proportional integral (GPI) controller based on the flatness theory that demonstrated good results in both stabilisation and tracking tasks, even in the presence of atmospheric disturbances and noise measurements, improving the performance of a traditional PID controller [16][17][18][19][20][21][22][23]. The theoretical details of the GPI control scheme are described in [15].…”
Section: Uav Simulatormentioning
confidence: 99%
“…Flapping-Wing: This class of micro-UAV reproduces the flight of birds or insects [47][48][49]. It has an extremely low payload capability and low endurance owing to its reduced size.…”
mentioning
confidence: 99%