Design of a Flight Stabilizer System for a Small Fixed Wing Unmanned Aerial Vehicle using System Identification
1st IFAC Workshop on Advances in Control and Automation Theory for Transportation Applications, ACATTA 2013, İstanbul, Türkiye, 16 - 17 Eylül 2013, cilt.1, ss.145-149, (Tam Metin Bildiri)
- Yayın Türü: Bildiri / Tam Metin Bildiri
- Cilt numarası: 1
- Doi Numarası: 10.3182/20130916-2-tr-4042.00012
- Basıldığı Şehir: İstanbul
- Basıldığı Ülke: Türkiye
- Sayfa Sayıları: ss.145-149
- Ankara Yıldırım Beyazıt Üniversitesi Adresli: Hayır
Özet
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. © IFAC.