Результаты исследований: Научные публикации в периодических изданиях › статья › Рецензирование
Aircraft control with anti-windup compensation. / Leonov, G. A.; Kuznetsov, N. V.; Pogromskii, A. Yu; Andrievskii, B. R.
в: Differential Equations, Том 48, № 13, 12.2012, стр. 1700-1720.Результаты исследований: Научные публикации в периодических изданиях › статья › Рецензирование
}
TY - JOUR
T1 - Aircraft control with anti-windup compensation
AU - Leonov, G. A.
AU - Kuznetsov, N. V.
AU - Pogromskii, A. Yu
AU - Andrievskii, B. R.
N1 - Funding Information: The research was supported by the Ministry of Education and Science of the Russian Federation, St. Petersburg State University, Academy of Finland, and the Russian Foundation for Basic Research (project no. 12-08-01183-a).
PY - 2012/12
Y1 - 2012/12
N2 - We consider an anti-windup compensation method ensuring the convergence of the closed-loop system for a class of reference signals. An application of the method to an aircraft flight control problem is shown.
AB - We consider an anti-windup compensation method ensuring the convergence of the closed-loop system for a class of reference signals. An application of the method to an aircraft flight control problem is shown.
KW - LOOP CONTROL-SYSTEMS
KW - HIDDEN OSCILLATIONS
KW - CONVERGENT SYSTEMS
KW - STABILITY ANALYSIS
KW - DESIGN
KW - PERFORMANCE
KW - ALGORITHMS
KW - SATURATION
KW - CIRCUITS
KW - AIZERMAN
UR - http://www.scopus.com/inward/record.url?scp=84874925769&partnerID=8YFLogxK
U2 - 10.1134/S0012266112130022
DO - 10.1134/S0012266112130022
M3 - Article
VL - 48
SP - 1700
EP - 1720
JO - Differential Equations
JF - Differential Equations
SN - 0012-2661
IS - 13
ER -
ID: 5487371