2023
DOI: 10.1016/j.ast.2023.108241
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Distributed bearing-based formation maneuver control of fixed-wing UAVs by finite-time orientation estimation

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Cited by 39 publications
(14 citation statements)
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“…Remark 4. Assumptions 3 and 4 are prevalent in the bearing-based formation control problem with a leader-follower structure [37][38][39]. Given that the formation controls designed are unavailable for the unique target formation, Assumption 3 is fundamental for the leader-follower structured UAV problem, as stipulated by Lemma 1.…”
Section: Problem Formulationmentioning
confidence: 99%
“…Remark 4. Assumptions 3 and 4 are prevalent in the bearing-based formation control problem with a leader-follower structure [37][38][39]. Given that the formation controls designed are unavailable for the unique target formation, Assumption 3 is fundamental for the leader-follower structured UAV problem, as stipulated by Lemma 1.…”
Section: Problem Formulationmentioning
confidence: 99%
“…Many efforts have been devoted to the finite-time consensus problem of systems with general linear [7], high-order integrator [8,9], other nonlinear dynamics such as typical Euler-Lagrange dynamics [10] and attitude consensus of spacecraft [11][12][13]. Compared with asymptotic control, which requires the system to converge to a given bound exponentially, a finite-time control law can lead to a faster convergence rate (near the equilibrium point) [14,15]. However, the convergent time resulting from finite-time control schemes heavily depends on the initial conditions.…”
Section: Introductionmentioning
confidence: 99%
“…Many researchers have attempted to investigate accident-contributing elements; however, little work has been given to explaining black box models [ 27 , 28 ]. The authors applied five machine learning models and explainable machine learning [ 29 , 30 ].…”
Section: Introductionmentioning
confidence: 99%