2017 IEEE/RSJ International Conference on Intelligent Robots and Systems (IROS) 2017
DOI: 10.1109/iros.2017.8206422
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Circular formation control of fixed-wing UAVs with constant speeds

Abstract: Abstract-In this paper we propose an algorithm for stabilizing circular formations of fixed-wing UAVs with constant speeds. The algorithm is based on the idea of tracking circles with different radii in order to control the inter-vehicle phases with respect to a target circumference. We prove that the desired equilibrium is exponentially stable and thanks to the guidance vector field that guides the vehicles, the algorithm can be extended to other closed trajectories. One of the main advantages of this approac… Show more

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Cited by 28 publications
(29 citation statements)
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“…Lemma 3: The zero vector 0 ∈ R n−1 is a regular value of the C 2 function e in (6), and hence the desired path P is a C 2 embedded submanifold 4 in R n .…”
Section: B General Guiding Vector Fieldmentioning
confidence: 99%
“…Lemma 3: The zero vector 0 ∈ R n−1 is a regular value of the C 2 function e in (6), and hence the desired path P is a C 2 embedded submanifold 4 in R n .…”
Section: B General Guiding Vector Fieldmentioning
confidence: 99%
“…To hold a formation, the MAVs must hold a relative position or distance between given neighbors, such that they can move as one unit through space. See, for instance, the works of Quintero et al ( 2013 ), Schiano et al ( 2016 ), de Marina et al ( 2017 ), Yuan et al ( 2017 ), and de Marina and Smeur ( 2019 ). One advantage of flying in formation for MAV swarms is their predictability during operations.…”
Section: Swarm-level Controlmentioning
confidence: 99%
“…For example, we can modify the nominal guiding vector field (5) in a minimally invasive way using safety barrier certificates [49], [50]. Specifically, we add an extra term u col i ∈ R n+1 to the vector field in (5), and this term is calculated by a quadratic program min u col i (t) 2 subject to the constraintsḂ ij (ξ i , ξ j ) ≤ 1/B ij (ξ i , ξ j ) for j = i and i, j ∈ Z N 1 , where B ij (ξ i , ξ j ) is a control barrier function [51] (e.g., B ij (ξ i , ξ j ) = 1/( p i − p j 2 − R 2 ), where p i is the physical position and R is the safe distance between robots). The collision avoidance behavior is shown in the supplementary video, but the theoretical analysis is left for future work.…”
Section: Convergence Analysismentioning
confidence: 99%
“…In this experiment, two autonomous fixed-wing aircraft (i.e., Autonomous Opterra 1.2m) similar to [5], [57] are employed to validate Theorem 2. The aircraft are equipped with the opensource software/hardware project Paparazzi [58].…”
Section: B Flights With Fixed-wing Aircraftmentioning
confidence: 99%