scheme and comprehensive utilization of missile-borne auxiliary energy
should be adopted as far as possible without affecting the performance of
energy user subsystems. Of course, this is not always the case because of
special requirements and conditions.
(6) The eccentric speed of the control surface depends on the instantaneous
change rate of the control command and the stable signal and the speed load
characteristics of the steering gear. The former is related to the design
Table 9.9 Additional conditions for the design of air defense missile control execution system
Distinguish
Serial
Number
Parameter
Explain
Remarks
Control
trajectory
1
Variation law of
control surface
deflection angle
Control surface deflection
change of typical control
trajectory
2
Law of moment
change on control
surface
Moment change of control
surface of typical control
trajectory
3
Law of change of
locking moment
Change of locking moment
of typical control trajectory
4
Energy level
conversion time
Interstage conversion time
of energy level I and II
Frequency
coupling
5
Controlling the
bending -torsion
frequency ratio of
actuator
Natural vibration frequency
ratio of bending and torsion
of control surface actuator
6
Natural vibration and
energy characteristic
frequency ratio of
mechanisms
Controlling surface actuator
torsional vibration
frequency and energy
characteristic frequency
ratio
Launch
and control
system
7
Energy start time
Time from energy start to
pressure establishment
Telemetry
system
8
Output signal of
rudder system
integrated amplifier
Using corresponding
telemetry additives
9
Control surface
torque
Using corresponding
telemetry sensor and
amplifier
10
Control plane
deflection
Using corresponding
telemetry sensors or
additives
11
Energy characteristic
parameters
For example, the pressure,
flow rate, temperature and
vibration of gas and liquid
energy sources; or current,
voltage, frequency of power
supply, etc.
80
9 High-Temperature and High-Speed Gas Turbine Pump …
should be adopted as far as possible without affecting the performance of
energy user subsystems. Of course, this is not always the case because of
special requirements and conditions.
(6) The eccentric speed of the control surface depends on the instantaneous
change rate of the control command and the stable signal and the speed load
characteristics of the steering gear. The former is related to the design
Table 9.9 Additional conditions for the design of air defense missile control execution system
Distinguish
Serial
Number
Parameter
Explain
Remarks
Control
trajectory
1
Variation law of
control surface
deflection angle
Control surface deflection
change of typical control
trajectory
2
Law of moment
change on control
surface
Moment change of control
surface of typical control
trajectory
3
Law of change of
locking moment
Change of locking moment
of typical control trajectory
4
Energy level
conversion time
Interstage conversion time
of energy level I and II
Frequency
coupling
5
Controlling the
bending -torsion
frequency ratio of
actuator
Natural vibration frequency
ratio of bending and torsion
of control surface actuator
6
Natural vibration and
energy characteristic
frequency ratio of
mechanisms
Controlling surface actuator
torsional vibration
frequency and energy
characteristic frequency
ratio
Launch
and control
system
7
Energy start time
Time from energy start to
pressure establishment
Telemetry
system
8
Output signal of
rudder system
integrated amplifier
Using corresponding
telemetry additives
9
Control surface
torque
Using corresponding
telemetry sensor and
amplifier
10
Control plane
deflection
Using corresponding
telemetry sensors or
additives
11
Energy characteristic
parameters
For example, the pressure,
flow rate, temperature and
vibration of gas and liquid
energy sources; or current,
voltage, frequency of power
supply, etc.
80
9 High-Temperature and High-Speed Gas Turbine Pump …