Full metadata record
DC pole | Hodnota | Jazyk |
---|---|---|
dc.contributor.author | Baránek, Radek | |
dc.contributor.author | Šolc, František | |
dc.contributor.editor | Pihera, Josef | |
dc.contributor.editor | Steiner, František | |
dc.date.accessioned | 2013-12-18T07:28:27Z | |
dc.date.available | 2013-12-18T07:28:27Z | |
dc.date.issued | 2013 | |
dc.identifier.citation | Electroscope. 2013, č. 5, EEICT + EDS. | cs |
dc.identifier.issn | 1802-4564 | |
dc.identifier.uri | http://147.228.94.30/images/PDF/Rocnik2013/Cislo5_2013/r7c5c1.pdf | |
dc.identifier.uri | http://hdl.handle.net/11025/6615 | |
dc.format | 6 s. | cs |
dc.format.mimetype | application/pdf | |
dc.language.iso | en | en |
dc.publisher | Západočeská univerzita v Plzni, Fakulta elektrotechnická | cs |
dc.relation.ispartofseries | Electroscope | cs |
dc.rights | © 2013 Electroscope. All rights reserved. | en |
dc.subject | odhad polohy | cs |
dc.subject | anténní systémy | cs |
dc.subject | elektrotechnická měření | cs |
dc.subject | simulace | cs |
dc.subject | multikoptéra | cs |
dc.title | Tuning of complementary filter attitude estimator using presice model of multicopter | en |
dc.type | článek | cs |
dc.type | article | en |
dc.rights.access | openAccess | en |
dc.type.version | publishedVersion | en |
dc.description.abstract-translated | This contribution deals with attitude estimation algorithm based on measuring angular rate, earth magnetic field and specific force and with the tuning of its parameters. At first, sensors and two main methods usually used for attitude estimation are described. Subsequently the particular form of complementary filter attitude estimator is shown. Then the tuning of algorithm’s parameters using brute force simulation is described. For this trajectory generated using precise model of multicopter was used. Testing trajectory reflects usual mission of unmanned aerial vehicles called waypoint navigation. Use of trajectory generated by model is convenient because of the knowledge of the true state variables, so the comparison through RMSE (Root Mean Square Error) value is possible. | en |
dc.subject.translated | attitude estimation | en |
dc.subject.translated | aerial systems | en |
dc.subject.translated | electrical measurements | en |
dc.subject.translated | simulation | en |
dc.subject.translated | multicopter | en |
dc.type.status | Peer-reviewed | en |
Vyskytuje se v kolekcích: | Číslo 5 (2013) Číslo 5 (2013) |
Soubory připojené k záznamu:
Soubor | Popis | Velikost | Formát | |
---|---|---|---|---|
r7c5c1.pdf | Plný text | 267,34 kB | Adobe PDF | Zobrazit/otevřít |
Použijte tento identifikátor k citaci nebo jako odkaz na tento záznam:
http://hdl.handle.net/11025/6615
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