Результаты исследований: Публикации в книгах, отчётах, сборниках, трудах конференций › статья в сборнике материалов конференции › научная › Рецензирование
Serial nonlinear correction method in the flight vehicle systems. / Кузнецов, Николай Владимирович; Андриевский, Борис Ростиславич; Зайцева, Юлия Сергеевна.
Cyber-Physical Systems and Control II: International Conference Cyber-Physical Systems and Control CPS&C 2021. Том 460 2023. стр. 315-324 (Lecture Notes in Networks and Systems; Том 460).Результаты исследований: Публикации в книгах, отчётах, сборниках, трудах конференций › статья в сборнике материалов конференции › научная › Рецензирование
}
TY - GEN
T1 - Serial nonlinear correction method in the flight vehicle systems
AU - Кузнецов, Николай Владимирович
AU - Андриевский, Борис Ростиславич
AU - Зайцева, Юлия Сергеевна
PY - 2023
Y1 - 2023
N2 - The nonlinear correction method is widely used in automatic control systems to increase stability margins and quality rating. This method has also found application in piloted aircraft control tasks, where the loss of stability and the occurrence of oscillations are unacceptable. This paper discusses new nonlinear correcting devices. Their structure is based on separate channels of the desired control signal amplitude and phase formation. Their application is demonstrated by the example of a piloted aircraft, the control systems of which have actuator rate limits. The illustrations of frequency characteristics, spectrograms of nonlinear correcting devices, time processes of the input, and actual signals of corrected and nonlinear uncorrected systems, from which the efficiency of the serial correcting devices are observable, are presented.
AB - The nonlinear correction method is widely used in automatic control systems to increase stability margins and quality rating. This method has also found application in piloted aircraft control tasks, where the loss of stability and the occurrence of oscillations are unacceptable. This paper discusses new nonlinear correcting devices. Their structure is based on separate channels of the desired control signal amplitude and phase formation. Their application is demonstrated by the example of a piloted aircraft, the control systems of which have actuator rate limits. The illustrations of frequency characteristics, spectrograms of nonlinear correcting devices, time processes of the input, and actual signals of corrected and nonlinear uncorrected systems, from which the efficiency of the serial correcting devices are observable, are presented.
KW - Altitude
KW - Filter
KW - Oscillations prevention
KW - Pilot model
KW - Pitch control
KW - Saturation
KW - Spacecraft
UR - https://www.mendeley.com/catalogue/201fd374-2894-3deb-9d70-2da69a26ad39/
U2 - 10.1007/978-3-031-20875-1_29
DO - 10.1007/978-3-031-20875-1_29
M3 - Conference contribution
SN - 9783031208744
VL - 460
T3 - Lecture Notes in Networks and Systems
SP - 315
EP - 324
BT - Cyber-Physical Systems and Control II
T2 - Cyber-Physical Systems and Control II: International Conference Cyber-Physical Systems and Control CPS&C 2021.
Y2 - 29 June 2021 through 2 July 2021
ER -
ID: 114461808