Lecture
1. Justify the choice of displacements of moving elements of hydromechanical systems of aircraft engine control systems (SU DLA) as state variables.
2. How is operating pressure accounted for in models of hydromechanical systems of aircraft engine control systems (SU DLA)?
3. At which design stages of an aircraft engine control system (SU DLA) can an element-by-element model be used?
4. Which dynamic variables in the hydromechanical systems of aircraft engine control systems (SU DLA) are unmeasurable, and why?
5. Identify the properties of the hydromechanical actuator (GMA) model.
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