Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › Research › peer-review
Hidden oscillations in aircraft flight control system with input saturation. / Andrievsky, B. R.; Kuznetsov, N. V.; Leonov, G. A.; Pogromsky, A. Yu.
5th IFAC International Workshop on Periodic Control Systems, PSYCO 2013 - Proceedings. 12 PART 1. ed. International Federation of Automatic Control, 2013. p. 75-79 (IFAC Proceedings Volumes (IFAC-PapersOnline); Vol. 46, No. 12 PART 1).Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › Research › peer-review
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TY - GEN
T1 - Hidden oscillations in aircraft flight control system with input saturation
AU - Andrievsky, B. R.
AU - Kuznetsov, N. V.
AU - Leonov, G. A.
AU - Pogromsky, A. Yu
N1 - Funding Information: This work was supported by the Academy of Finland, Russian Ministry of Education and Science (Federal target programm), Russian Foundation for Basic Research and Saint-Petersburg State University.
PY - 2013
Y1 - 2013
N2 - The presence of actuator saturation can dramatically degrade the system performance. Since the feedback loop is broken when the actuator saturates the unstable modes of the regulator may then drift to undesirable values. The consequences are that undesired nonlinear oscillations appear and that the settling time may unacceptably increase. Rigorous analysis of nonlinear aircraft models is a very difficult task, that is why a numerical simulation is often used as an analysis and design tool. In this paper difficulties of numerical analysis related to the existence of hidden oscillations in the aircraft control system are demonstrated.
AB - The presence of actuator saturation can dramatically degrade the system performance. Since the feedback loop is broken when the actuator saturates the unstable modes of the regulator may then drift to undesirable values. The consequences are that undesired nonlinear oscillations appear and that the settling time may unacceptably increase. Rigorous analysis of nonlinear aircraft models is a very difficult task, that is why a numerical simulation is often used as an analysis and design tool. In this paper difficulties of numerical analysis related to the existence of hidden oscillations in the aircraft control system are demonstrated.
KW - Aircraft
KW - Antiwindup
KW - Control
KW - Describing function
KW - Hidden oscillations
KW - Saturation
UR - http://www.scopus.com/inward/record.url?scp=84886823072&partnerID=8YFLogxK
U2 - 10.3182/20130703-3-FR-4039.00026
DO - 10.3182/20130703-3-FR-4039.00026
M3 - Conference contribution
SN - 9783902823380
T3 - IFAC Proceedings Volumes (IFAC-PapersOnline)
SP - 75
EP - 79
BT - 5th IFAC International Workshop on Periodic Control Systems, PSYCO 2013 - Proceedings
PB - International Federation of Automatic Control
T2 - 5th IFAC International Workshop on Periodic Control Systems, PSYCO 2013
Y2 - 3 July 2013 through 5 July 2013
ER -
ID: 7410418