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01098naa a2200313 i 4500 |
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HR-ZaNSK |
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20200114084618.0 |
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ta |
| 008 |
200114s2017 ci | |0|| ||eng |
| 035 |
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|a (HR-ZaNSK)001052070
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| 040 |
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|a HR-ZaNSK
|b hrv
|c HR-ZaNSK
|e ppiak
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| 042 |
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|a croatica
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| 044 |
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|a ci
|c hr
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| 080 |
1 |
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|a 629
|2 2011
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| 080 |
1 |
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|a 51
|2 2011
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| 100 |
1 |
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|a Ying-hui, Li
|4 aut
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| 245 |
1 |
0 |
|a Stability region of closed-loop pilot-vehicle system for fly-by-wire aircraft with limited actuator rate /
|c Li Ying-hui, Qu Liang, Xu Hao-jun, Cao Qi-meng.
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| 300 |
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|b Ilustr.
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| 504 |
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|a Bibliografija: 15 jed.
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| 504 |
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|a Abstract.
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| 653 |
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0 |
|a Letjelica
|a Aktuator
|a Stabilnost
|a Analiza stabilnosti
|a Nelinearni model
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| 700 |
1 |
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|a Liang, Qu
|4 aut
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| 700 |
1 |
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|a Hao-jun, Xu
|4 aut
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| 700 |
1 |
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|a Qi-meng, Cao
|4 aut
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| 773 |
0 |
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|t Engineering review (Technical Faculty University of Rijeka)
|x 1330-9587
|g 37 (2017), 3 ; str. 263-271
|w nsk.(HR-ZaNSK)000166773
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| 981 |
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|b B06/17
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| 998 |
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|b rpeo2001
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| 856 |
4 |
1 |
|u https://hrcak.srce.hr/184815
|y Elektronička verzija članka
|