2015
DOI: 10.2322/tjsass.58.187
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Dynamics and Simulation of the Effects of Wind on UAVs and Airborne Wind Measurement

Abstract: This paper presents a simulation of wind effects on a flying unmanned aerial vehicle (UAV) and a simulation of wind measurements taken from an airborne UAV. The wind acts as a disturbance on the flying UAV by altering its attitude and velocity. Therefore, the airborne measurement should be taken dynamically to reflect the instantaneous motion of a vehicle that is affected by wind. In order to understand and validate the algorithm that measures wind and the interaction between wind and the UAV, an investigation… Show more

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Cited by 21 publications
(16 citation statements)
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“…Another commonly studied testbed uses a proportional-embedded PID controller to jointly control position and attitude [1,2,3,12,13]. The AscTec Hummingbird is a typical model of this type of quadrotor.…”
Section: Control Systems For Unmanned Aerial Vehicles Uavsmentioning
confidence: 99%
“…Another commonly studied testbed uses a proportional-embedded PID controller to jointly control position and attitude [1,2,3,12,13]. The AscTec Hummingbird is a typical model of this type of quadrotor.…”
Section: Control Systems For Unmanned Aerial Vehicles Uavsmentioning
confidence: 99%
“…In practice, due to, e.g., imperfect channel estimation and finite feedback, the UAVs can never have perfect CSI. Moreover, the wind would incur non-negligible body jittering of the UAVs, which will also harm the acquisition of CSI [19]. Therefore, it is of great importance to investigate the robust system design of UAV assisted wireless communication system under imperfect CSI assumptions.…”
Section: Index Termsmentioning
confidence: 99%
“…where K = max{N m , ∀m ∈ M} and θ nmi = 0 for N n < i ≤ K, ∀n, m ∈ M. (20a) collects all the inter-cell interferences, while (20b) contains [Θ n1 , ..., Θ n K ] and {θ nm K } m, K (where m = n) that are relevant to UAV n . Remind that Θ n K = Nm m=1,m =n θ mn K , it can be verified that there exists a matrix E n ∈ {0, 1} M K×M M K , such that θ n = E n θ, ∀n ∈ M. Then, based on (19) and (20), problem (18) can be compactly rewritten as…”
Section: Nn K=1mentioning
confidence: 99%
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“…In practical UAV communication systems, UAV-mounted transceivers flying in the air may encounter strong wind gusts, which leads to random body jittering with respect to angular movements [7]. The estimation accuracy of the D. Xu, Y.…”
Section: Introductionmentioning
confidence: 99%