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Wyszukujesz frazę "dynamic parameters" wg kryterium: Temat


Wyświetlanie 1-3 z 3
Tytuł:
Estimation of speed dependent fault parameters in a coupled rotor-bearing system
Autorzy:
Lal, M.
Satapathy, M.
Powiązania:
https://bibliotekanauki.pl/articles/140014.pdf
Data publikacji:
2018
Wydawca:
Polska Akademia Nauk. Czytelnia Czasopism PAN
Tematy:
speed-dependent dynamic parameters
rotor-bearing-coupling
misalignment
analytical approach
multiple faults
Lagrange's method
parametry dynamiczne zależne
wirnik-łożysko-sprzęgło
niewspółosiowość
podejście analityczne
błędy wielokrotne
metoda Lagrange'a
Opis:
In rotating machineries, misalignment is considered as the second most major cause of failure after unbalance. In this article, model-based multiple fault identification technique is presented to estimate speed-dependent coupling misalignment and bearing dynamic parameters in addition with speed independent residual unbalances. For brevity in analysis, a simple coupled rotor bearing system is considered and analytical approach is used to develop the identification algorithm. Equations of motion ingeneralized co-ordinates are derived with the help of Lagrange’s equation and least squares fitting approach is used to estimate the speed-dependent fault parameters. Present identification algorithm requires independent sets of forced response data which are generated with the help of different sets of trial unbalances. To avoid/suppress the ill-conditioning of regression equation, independent sets of forced response data are obtained by rotating the rotor in clock-wise and counter clock-wise directions, alternatively. Robustness of algorithm is checked for different levels of measurement noise.
Źródło:
Archive of Mechanical Engineering; 2018, LXV, 3; 327-347
0004-0738
Pojawia się w:
Archive of Mechanical Engineering
Dostawca treści:
Biblioteka Nauki
Artykuł
Tytuł:
Longitudinal automatic carrier-landing control law rejecting disturbances and coupling based on adaptive dynamic inversion
Autorzy:
Wang, Lipeng
Zhang, Zhi
Zhu, Qidan
Wen, Zixia
Powiązania:
https://bibliotekanauki.pl/articles/2090730.pdf
Data publikacji:
2021
Wydawca:
Polska Akademia Nauk. Czytelnia Czasopism PAN
Tematy:
carrier-based aircraft
automatic landing
nonlinear dynamic inversion
lateral decoupling
parameters adaptation
statki powietrzne bazujące na lotniskowcach
automatyczne lądowanie
inwersja dynamiczna nieliniowa
odsprzęganie boczne
dostosowanie parametrów
Opis:
The longitudinal automatic carrier landing system (ACLS) control law is designed based on nonlinear dynamic inversion (NDI), which can reject air wake, decouple lateral states, and track the dynamic desired touchdown point (DTP). First of all, the nonlinear landing model of F/A−18 aircraft in the final approach is established, in which the parameters of the aerodynamic, control surfaces, and limited states are acquired. Second, the strategy of tracking the desired longitudinal trajectory through pitch angle control is adopted. The automatic power compensation system (APCS), pitch angle rate, pitch angle, and vertical position control loops are developed based on the adaptive NDI. The stable analysis and the principal description are derived in detail. Deck motion compensation (DMC) algorithm is designed by frequency response method. Third, the control parameters are optimized through the genetic algorithm. A fitness function integrated with velocity, angle of attack (AOA), pitch rate, pitch angle, and vertical position of the aircraft are proposed. Finally, integrated simulations are conducted on a semi-physical simulation platform. The results indicate that the adopted automatic landing control law can achieve both excellent performance and the ability to reject the air wake and lateral coupling.
Źródło:
Bulletin of the Polish Academy of Sciences. Technical Sciences; 2021, 69, 1; e136217, 1--10
0239-7528
Pojawia się w:
Bulletin of the Polish Academy of Sciences. Technical Sciences
Dostawca treści:
Biblioteka Nauki
Artykuł
Tytuł:
Longitudinal automatic carrier-landing control law rejecting disturbances and coupling based on adaptive dynamic inversion
Autorzy:
Wang, Lipeng
Zhang, Zhi
Zhu, Qidan
Wen, Zixia
Powiązania:
https://bibliotekanauki.pl/articles/2173584.pdf
Data publikacji:
2021
Wydawca:
Polska Akademia Nauk. Czytelnia Czasopism PAN
Tematy:
carrier-based aircraft
automatic landing
nonlinear dynamic inversion
lateral decoupling
parameters adaptation
statki powietrzne bazujące na lotniskowcach
automatyczne lądowanie
inwersja dynamiczna nieliniowa
odsprzęganie boczne
dostosowanie parametrów
Opis:
The longitudinal automatic carrier landing system (ACLS) control law is designed based on nonlinear dynamic inversion (NDI), which can reject air wake, decouple lateral states, and track the dynamic desired touchdown point (DTP). First of all, the nonlinear landing model of F/A−18 aircraft in the final approach is established, in which the parameters of the aerodynamic, control surfaces, and limited states are acquired. Second, the strategy of tracking the desired longitudinal trajectory through pitch angle control is adopted. The automatic power compensation system (APCS), pitch angle rate, pitch angle, and vertical position control loops are developed based on the adaptive NDI. The stable analysis and the principal description are derived in detail. Deck motion compensation (DMC) algorithm is designed by frequency response method. Third, the control parameters are optimized through the genetic algorithm. A fitness function integrated with velocity, angle of attack (AOA), pitch rate, pitch angle, and vertical position of the aircraft are proposed. Finally, integrated simulations are conducted on a semi-physical simulation platform. The results indicate that the adopted automatic landing control law can achieve both excellent performance and the ability to reject the air wake and lateral coupling.
Źródło:
Bulletin of the Polish Academy of Sciences. Technical Sciences; 2021, 69, 1; art. no. e136217
0239-7528
Pojawia się w:
Bulletin of the Polish Academy of Sciences. Technical Sciences
Dostawca treści:
Biblioteka Nauki
Artykuł
    Wyświetlanie 1-3 z 3

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