Reduced Actuator Set for Pressure Control and Thrust Distribution for Multinozzle Propulsion Systems

Table 4

Simulation conditions.

Property	Values
Amp gain	0.7407
Servo valve gain
PID controller gain
	10
	5
	5
Initial chamber volume,
Discharge coefficient	0.611
Fluid density	867
Bulk modulus
Supply pressure
Return pressure	0
Valve inlet/outlet area
Piston area