2008 IEEE Instrumentation and Measurement Technology Conference 2008
DOI: 10.1109/imtc.2008.4547087
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Pythagorean Hodograph (PH) Path Planning for Tracking Airborne Contaminant using Sensor Swarm

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Cited by 22 publications
(16 citation statements)
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“…The theory of rational adapted RMFs on general spatial PH curves yields results analogous to (32) and (33), but without the sin θ factor in (33). In the absence of this factor, the rotation matrix in (32) is rational in ξ, and hence the RMF (f 1 , f 2 , f 3 ) is rational.…”
mentioning
confidence: 79%
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“…The theory of rational adapted RMFs on general spatial PH curves yields results analogous to (32) and (33), but without the sin θ factor in (33). In the absence of this factor, the rotation matrix in (32) is rational in ξ, and hence the RMF (f 1 , f 2 , f 3 ) is rational.…”
mentioning
confidence: 79%
“…There has recently been considerable interest in using Pythagorean-hodograph (PH) curves to specify paths for swarms of unmanned aerial vehicles (UAVs) or other autonomous or remotely-operated vehicles [1,3,4,6,20,21,23,24,25,26,27,28,29,30,31,33]. A polynomial PH curve r(ξ) = (x(ξ), y(ξ), z(ξ)) incorporates a special algebraic structure [9], ensuring that the components of the hodograph (derivative) r ′ (ξ) = (x ′ (ξ), y ′ (ξ), z ′ (ξ)) satisfy a Pythagorean condition -i.e., x ′2 (ξ)+y ′2 (ξ)+z ′2 (ξ) is equal to the perfect square of a single polynomial.…”
Section: Introductionmentioning
confidence: 99%
“…In (11) the paths are allowed to intersect, but the vehicles are time separated and hence do not arrive at the intersection point simultaneously. If either Equation (10) or (11) is satisfied, then the generated trajectories are spatially deconflicted and therefore form a set of feasible paths. In this paper, feasible paths are generated by imposing the spatial separation constraint (Equation (10)); ensuring minimal spatial clearance E between the paths through temporal separation is part of ongoing research.…”
Section: Trajectory Generationmentioning
confidence: 99%
“…subject to boundary conditions (6), dynamic constraints of the aircraft (8), mission-specific constraints, for example Equation (9), Equation (10) or (11) for spatial deconfliction,…”
Section: Trajectory Generationmentioning
confidence: 99%
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