2015
DOI: 10.3390/app5041457
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Quantum Wind Driven Optimization for Unmanned Combat Air Vehicle Path Planning

Abstract: Unmanned combat air vehicle (UCAV) path planning aims to calculate the optimal or suboptimal flight path considering the different threats and constraints under the complex battlefield environment. This flight path can help the UCAV avoid enemy threats and improve the efficiency of the investigation. This paper presents a new quantum wind driven optimization (QWDO) for the path planning of UCAV. QWDO algorithm uses quantum rotation gate strategy on population evolution and the quantum non-gate strategy to real… Show more

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Cited by 17 publications
(10 citation statements)
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References 19 publications
(29 reference statements)
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“…To increase the level of autonomy and reduce the dependencies on manual operators, various planning and control strategies have been developed regarding the problem of target tracking, target acquisition, disaster rescue and so on [2][3][4]. As one of the most complicated and important problems, the target tracking is regarded as a guidance law problem in this paper, assuming the target motion to be observed in the monitoring range.…”
Section: Introductionmentioning
confidence: 99%
“…To increase the level of autonomy and reduce the dependencies on manual operators, various planning and control strategies have been developed regarding the problem of target tracking, target acquisition, disaster rescue and so on [2][3][4]. As one of the most complicated and important problems, the target tracking is regarded as a guidance law problem in this paper, assuming the target motion to be observed in the monitoring range.…”
Section: Introductionmentioning
confidence: 99%
“…Improved ACO [14,15], A* and Theta* [16] algorithms are used for route planning in three-dimensional environments. To improve the investigation efficiency of unmanned bombs, scholars have proposed the Quantum Wind Driven [17] algorithm. Scholars have proposed a variety of optimization and improvement methods for the route planning problem under different conditions and have solved these problems relatively well.…”
Section: Introductionmentioning
confidence: 99%
“…(2) where v 0 is UAV cruise velocity. Respectively, v max and ω max are UAV velocity and turn rate maximal variation ranges.…”
Section: Uav Dynamic Modelmentioning
confidence: 99%
“…u = (u v , u ω ) T is velocity and turn rate control command constrained by fixed-wing UAV dynamic model [26] in Equation (2).…”
Section: Uav Dynamic Modelmentioning
confidence: 99%
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