Результаты исследований: Научные публикации в периодических изданиях › статья в журнале по материалам конференции › Рецензирование
Convergence-based analysis of robustness to delay in anti-windup loop of aircraft autopilot. / Andrievsky, Boris; Kuznetsov, Nikolay; Leonov, Gennady.
в: IFAC-PapersOnLine, Том 28, № 9, 01.07.2015, стр. 144-149.Результаты исследований: Научные публикации в периодических изданиях › статья в журнале по материалам конференции › Рецензирование
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TY - JOUR
T1 - Convergence-based analysis of robustness to delay in anti-windup loop of aircraft autopilot
AU - Andrievsky, Boris
AU - Kuznetsov, Nikolay
AU - Leonov, Gennady
PY - 2015/7/1
Y1 - 2015/7/1
N2 - The windup phenomenon is interpreted as a consequence of the convergent property absence for system with a saturation. This makes it possible to use the frequency-domain criterion for analysis of anti-windup augmentation in the case of stable and marginally stable plants. Based on this approach, robustness of the systems with respect to time delay in the anti-windup loop is examined and the approach for an optimal choice of the static anti-windup gain is proposed. An application of the convergence-based anti-windup control strategy to aircraft flight control for the case of time-delay in the anti-windup loop is described and studied by simulations.
AB - The windup phenomenon is interpreted as a consequence of the convergent property absence for system with a saturation. This makes it possible to use the frequency-domain criterion for analysis of anti-windup augmentation in the case of stable and marginally stable plants. Based on this approach, robustness of the systems with respect to time delay in the anti-windup loop is examined and the approach for an optimal choice of the static anti-windup gain is proposed. An application of the convergence-based anti-windup control strategy to aircraft flight control for the case of time-delay in the anti-windup loop is described and studied by simulations.
KW - Anti-windup correction
KW - Convergent systems
KW - Flight control
KW - Integrator windup
UR - http://www.scopus.com/inward/record.url?scp=84992520710&partnerID=8YFLogxK
U2 - 10.1016/j.ifacol.2015.08.074
DO - 10.1016/j.ifacol.2015.08.074
M3 - Conference article
AN - SCOPUS:84992520710
VL - 28
SP - 144
EP - 149
JO - IFAC-PapersOnLine
JF - IFAC-PapersOnLine
SN - 2405-8963
IS - 9
T2 - 1st IFAC Workshop on Advanced Control and Navigation for Autonomous Aerospace Vehicles, ACNAAV 2015
Y2 - 10 June 2015 through 12 June 2015
ER -
ID: 41251412