2018
DOI: 10.21278/tof.42101
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Chattering-Free Tracking Control of a Fully Actuated Multirotor with Passively Tilted Rotors

Abstract: SummaryIn this paper, a control allocation scheme is presented for a multirotor type of an Unmanned Aerial Vehicle (UAV). The control allocation scheme depends on the multirotor configuration and rotor system parameters, and it enables analysis of dynamics of different multirotor designs depending on the purpose and the task which the multirotor has to carry out. The analysis of force and moment distribution in space shows that the non-flat design with passively tilted rotors can overcome an inherent underactu… Show more

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Cited by 11 publications
(8 citation statements)
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“…The first step in the algebraic observer design is also the annihilation of initial conditions. The annihilation operator (18) with the real frequency shift is used in combination with the similar invariant filtering procedure as in Subsection 3.2.…”
Section: Fsb Algebraic Observermentioning
confidence: 99%
See 1 more Smart Citation
“…The first step in the algebraic observer design is also the annihilation of initial conditions. The annihilation operator (18) with the real frequency shift is used in combination with the similar invariant filtering procedure as in Subsection 3.2.…”
Section: Fsb Algebraic Observermentioning
confidence: 99%
“…In , a design and control of fully actuated passively tilted multirotor are proposed. The non‐flat design with passively tilted rotors can overcome the inherent underactuated property of the flat multirotor configurations, as shown in Figure .…”
Section: Multirotor Dynamic Modelmentioning
confidence: 99%
“…Rotors can be rotated around two axes, either actively or passively, so it is important to define Generalized Control Allocation Scheme for Multirotor Type of UAVs http://dx.doi.org/10.5772/intechopen.73006 a geometric arrangement for different designs. Those configurations can be classified as nonflat multirotor configurations (NFMRC) [21].…”
Section: Nonconventional Propulsion Arrangementsmentioning
confidence: 99%
“…The assumption is that the position of the rotor lies in the X B Y B plane, so the third coordinate equals zero, Figure 6. Rotor coordinate systems [21]. Drones -Applications…”
Section: Rotor Unit Positionmentioning
confidence: 99%
“…A frame for handling of the path with zero curvature and reducing the complexity of the control law was introduced and the controller design had been achieved by transverse feedback linearization and a parallel transport frame [9]. A robust chattering-free sliding mode asymptotic tracking control design is presented for a fully actuated multirotor [10]. A disturbance observer-based model predictive controller is designed for image-based visual servoing of underwater vehicles subject to field-of view constraint, actuator saturation, and external disturbances [11].…”
Section: Introductionmentioning
confidence: 99%