2015
DOI: 10.1016/j.mechatronics.2015.06.006
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Systems design and implementation with jerk-optimized trajectory generation for UAV calligraphy

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Cited by 30 publications
(12 citation statements)
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References 36 publications
(33 reference statements)
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“…In this mode, we initially minimize the jerk to obtain a trajectory which facilitates adequate tag acquisition by (implicitly) minimizing motion blur on the vision-based target detection. Such minimum jerk approach produces smooth trajectories and has a long heritage for planning MAV paths [5,24,25]. As the UAV approaches the target, the effect of disturbances increases so the planner minimizes the time spent in the turbulent area.…”
Section: B Dynamic Landing Plannermentioning
confidence: 99%
“…In this mode, we initially minimize the jerk to obtain a trajectory which facilitates adequate tag acquisition by (implicitly) minimizing motion blur on the vision-based target detection. Such minimum jerk approach produces smooth trajectories and has a long heritage for planning MAV paths [5,24,25]. As the UAV approaches the target, the effect of disturbances increases so the planner minimizes the time spent in the turbulent area.…”
Section: B Dynamic Landing Plannermentioning
confidence: 99%
“…Jerk in technical pain [177]; 20. Jerk in unmanned aerial vehicle (UAV) [11,[178][179][180][181][182][183][184][185][186]; and 21. Jerk in vehicles (ride comfort [12,15,17,19,25,45,95,98-106,108,109,111-113,115,118-121, 123-125,127-131], anti-jerk controller design [95,[98][99][100][101][102]109,111,119,120,130], autonomous vehicles [12,16,114,123,187,188], and other [111,187,[189][190][191][192][193][194][195].…”
Section: Categorisation Of Jerk Applicationsmentioning
confidence: 99%
“…Quadcopters are known for their highly nonlinear motion dynamics and so nonlinear models are indispensable. A common practical procedure is to linearize the nonlinear quadcopter dynamic model around a hovering mode (the operating steady-state) since, due to its symmetric frame, the linear dynamic model becomes somewhat simplified, and therefore, it is easier to design linear controllers; see ( [26][27][28][29][30], [39]). A drawback of such linearized model, however, is the operation in the immediate proximity of the linearizing state point (hovering mode) must be secured.…”
Section: T mentioning
confidence: 99%
“… Namely, the 6-DoF flying object could not be controlled with a single loop, and thus, a cascade control system is indispensable. In order to recover and keep vicinity of the aforementioned hovering mode, there are various control approaches developed under the cascade control concept, where the inner loop ought to be designed at least 5 times faster than the outer loop; see [27]- [30], [39].…”
Section: T mentioning
confidence: 99%