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</script>handle: 2117/134073 , 10261/202282
Abstract This paper presents the design of a state observer which guarantees quadratic boundedness of the estimation error. By using quadratic Lyapunov stability analysis, the convergence rate and the ultimate (steady-state) error bounding ellipsoid are identified as the parameters that define the behaviour of the estimation. Then, it is shown that these objectives can be merged in a scalarised objective function with one design parameter, making the design problem convex. In the second part of the article, a UAV model is presented which can be made linear by considering a particular state and frame of reference. The UAV model is extended to incorporate a disturbance model of variable size. The joint model matches the structure required to derive an observer, following the lines of the proposed design approach. An observer for disturbances acting on the UAV is derived and the analysis of the performances with respect to the design parameters is presented. The effectiveness and main characteristics of the proposed approach are shown using simulation results.
Unmanned aerial vehicles (UAVs), Automatic control, :Informàtica::Automàtica i control [Àrees temàtiques de la UPC], Optimal estimation and filtering, disturbance estimation, Avions no tripulats, QA75.5-76.95, optimal estimation and filtering, Disturbance estimation, Unmanned aerial vehicles, unmanned aerial vehicles (uavs), Control automàtic, Electronic computers. Computer science, Àrees temàtiques de la UPC::Informàtica::Automàtica i control, QA1-939, System modelling, unmanned aerial vehicles (UAVs), system modelling, Mathematics, Drone aircraft
Unmanned aerial vehicles (UAVs), Automatic control, :Informàtica::Automàtica i control [Àrees temàtiques de la UPC], Optimal estimation and filtering, disturbance estimation, Avions no tripulats, QA75.5-76.95, optimal estimation and filtering, Disturbance estimation, Unmanned aerial vehicles, unmanned aerial vehicles (uavs), Control automàtic, Electronic computers. Computer science, Àrees temàtiques de la UPC::Informàtica::Automàtica i control, QA1-939, System modelling, unmanned aerial vehicles (UAVs), system modelling, Mathematics, Drone aircraft
| citations This is an alternative to the "Influence" indicator, which also reflects the overall/total impact of an article in the research community at large, based on the underlying citation network (diachronically). | 13 | |
| popularity This indicator reflects the "current" impact/attention (the "hype") of an article in the research community at large, based on the underlying citation network. | Top 10% | |
| influence This indicator reflects the overall/total impact of an article in the research community at large, based on the underlying citation network (diachronically). | Top 10% | |
| impulse This indicator reflects the initial momentum of an article directly after its publication, based on the underlying citation network. | Top 10% |
| views | 64 | |
| downloads | 102 |

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