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Design of a Flight Stabilizer System for a Small Fixed Wing Unmanned Aerial Vehicle using System Identification
| Content Provider | Semantic Scholar |
|---|---|
| Author | Korkmaz, Halim Ertin, Onur Baki Kasnakoğlu, Coşku Kaynak, Unver |
| Copyright Year | 2013 |
| Abstract | Abstract Flight stabilizers for unmanned aerial vehicles (UAVs) provide level flight and make the UAVs more reliable and operational. In this paper a system identification process is applied to flight data logs obtained from flight simulations and a stabilizer system is designed using the dynamical model obtained from system identification. Hardware-in-the-loop testing was also performed on the flight stabilizer system designed is also tested using a custom built moving platform in the pitch and roll axis with actual flight sensors. |
| Starting Page | 145 |
| Ending Page | 149 |
| Page Count | 5 |
| File Format | PDF HTM / HTML |
| DOI | 10.3182/20130916-2-TR-4042.00012 |
| Volume Number | 46 |
| Alternate Webpage(s) | https://kasnakoglu.files.wordpress.com/2013/09/designing-a-flight-stabilizer-02.pdf |
| Alternate Webpage(s) | https://doi.org/10.3182/20130916-2-TR-4042.00012 |
| Language | English |
| Access Restriction | Open |
| Content Type | Text |
| Resource Type | Article |
