2019
DOI: 10.1051/itmconf/20192401006
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Examination of the Unmanned Aerial Vehicle

Abstract: The contemporary interdisciplinary field of knowledge, which is the robotics used in unmanned aerial vehicles, is developing very dynamically. In view of the above, the authors of this paper have set themselves the following thesis: it is possible to build a flying mobile robot based on a controller with low computing power and a simple PID controller, and in this respect they undertook to prove it. The examined object in real experiments was the Quadrocopter. The article discusses the tasks implemented during… Show more

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Cited by 5 publications
(7 citation statements)
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“…The receiver clock error dtk r Tand carrier phase deviation dt , k r j Tare typical errors in Equation (14) and Equation (15), so they can be reduced by positioning DD. Therefore, this is the main reason why the DD positioning is preferably used.…”
Section: Static Experiments Based On a Gps+glonass System Receivermentioning
confidence: 99%
“…The receiver clock error dtk r Tand carrier phase deviation dt , k r j Tare typical errors in Equation (14) and Equation (15), so they can be reduced by positioning DD. Therefore, this is the main reason why the DD positioning is preferably used.…”
Section: Static Experiments Based On a Gps+glonass System Receivermentioning
confidence: 99%
“…Unmanned Aerial Vehicles (UAVs), commonly known as "drones, " are measurement platforms collecting data while flying over the area of interest ( Figure 1O). For operations in marine and coastal environments, different types of UAVs are used with varying flight duration and modes of operation (autonomous or manual; Colefax et al, 2017;Setlak and Kowalik, 2019). In marine monitoring UAVs can be used to increase the spatio-temporal resolution and coverage of monitoring data for parameters used to assess biodiversity, eutrophication, commercial fish and shellfish, hydrological conditions, contaminants and marine litter.…”
Section: Remote Sensingmentioning
confidence: 99%
“…Despite the fact that by using a traditional linearquadratic regulator, it is possible to achieve an increase in aircraft stability, however, information on all system state variables and large workloads are necessary, which is not conducive to using this method in practical applications [13], [14], [15].…”
Section: Feedback System (Output)mentioning
confidence: 99%
“…Because equation (13) must meet all initial conditions, all trajectories of state (0) satisfy the following Lapunov equation (15):= + + * + * = 0 (15) From equation (15) it can be stated that if and matrices are given, the auxiliary matrix can be determined by the Lapunov function and is independent of the state of the system.…”
Section: Feedback System (Output)mentioning
confidence: 99%
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