4. The dynamics of servo drives
Organization:
Page: Kosm. teh. Raket. vooruž. 2024, (1); 29-39
DOI: https://doi.org/10.33136/stma2024.01.029
Language: Ukrainian
Annotation: The article gives the analysis results for the servo drives dynamics, obtained from the theoretical calculations
and during the development testing of the high power electric drives. Theoretical research was conducted,
using the complete mathematical model of the servo drive, which included the equations of the control
signal shaping path, electric motor, reducer and load. The equations of the control signal shaping network
include only the characteristics of the compensating element in the assumption that all other delays in the
transformation path are minimized. The electric motor equations are assumed in the classical form, taking into
account the influence of the following main parameters on the motor dynamics: inductance and stator winding
resistance, torque and armature reaction coefficients and rotor moment of inertia. Interaction of the motor with
the multimass system of the reducer and load is presented in the form of force interaction of two masses –
a reduced mass of the rotor and mass of the load through the certain equivalent rigidity of the kinematic chain.
To describe the effect of gap in the kinematic connection the special computational trick, which considerably
simplifies its mathematical description, is used. Efficiency of the reducer is presented in the form of the internal
friction, proportional to the transmitted force. Calculation results with the application of the given mathematical
model match well with the results of the full-scale testing of different specimens of servo drives, which makes
it possible to use it for the development of new servomechanisms, as well as for the correct flight simulation
when testing the aircraft control systems. In particular, based on the frequency response calculations of the
closed circuit with the application of the given mathematical model, it is possible to define optimal parameters
of the correcting circuit. Reaction on the step action with the various values of circular amplification coefficient
in the circuit gives complete information on the stability regions of the closed circuit and influence of various
drive parameters on these regions. Based on the conducted theoretical and experimental studies, the basic
conclusions and recommendations were obtained and presented, accounting and implementation of which will
provide high dynamic characteristics of the newly designed servo drives.
Key words: electric drive, servo drive, reducer, stability, mathematical model.
Bibliography:
- Kozak L. Dynamika servomechanismov raketnoy techniki. Inzhenernye metody issledovaniya. Izd-vo LAP LAMBERT Academic Publiching, Germania. 2022.
- Kozak L. R., Shakhov M. I. Matematicheskie modely hydravlicheskikh servomekhanismov raketno-kosmicheskoy techniki. Kosmicheskaya technika. Raketnoe vooruzhenie. 2019. Vyp. 1.
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