Active control of a non-linear landing gear system having oleo pneumatic shock absorber using robust linear quadratic regulator approach
Proceedings Of The Institution Of Mechanical Engineers Part G-Journal Of Aerospace Engineering, cilt.232, sa.13, ss.2397-2411, 2018 (SCI-Expanded, Scopus)
- Yayın Türü: Makale / Tam Makale
- Cilt numarası: 232 Sayı: 13
- Basım Tarihi: 2018
- Dergi Adı: Proceedings Of The Institution Of Mechanical Engineers Part G-Journal Of Aerospace Engineering
- Derginin Tarandığı İndeksler: Science Citation Index Expanded (SCI-EXPANDED), Scopus
- Sayfa Sayıları: ss.2397-2411
- Yıldız Teknik Üniversitesi Adresli: Evet