1 sine vibration vibrationdata unit 2. 2 vibrationdata sine amplitude metrics

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1

Sine Vibration

VibrationdataVibrationdataUnit 2

2

VibrationdataVibrationdataSine Amplitude Metrics

3

Question

Does sinusoidal vibration ever occur in rocket vehicles?

VibrationdataVibrationdata

4

Space Shuttle, 4-segment booster 15 Hz

Ares-I, 5-segment booster 12 Hz

VibrationdataVibrationdataSolid Rocket Booster, Thrust Oscillation

5

Main Engine Cutoff (MECO)Transient at ~120 Hz

MECO could be a high force input to spacecraft

VibrationdataVibrationdataDelta II

6

The Pegasus launch vehicle oscillates

as a free-free beam during the 5-

second drop, prior to stage 1 ignition.

The fundamental bending frequency is

9 to 10 Hz, depending on the

payload’s mass & stiffness properties.

VibrationdataVibrationdataPegasus XL Drop Transient

7

-2.5

-2.0

-1.5

-1.0

-0.5

0

0.5

1.0

1.5

2.0

2.5

0 0.5 1.0 1.5 2.0 2.5 3.0 3.5 4.0

y=1.55*exp(-0.64*(x-0.195))Flight Data

damp = 1.0%fn = 9.9 Hz

TIME (SEC)

AC

CE

L (

G)

PEGASUS REX2 S3-5 PAYLOAD INTERFACE Z-AXIS5 TO 15 Hz BP FILTERED

VibrationdataVibrationdataPegasus XL Drop Transient Data

8

Pogo

Pogo is the popular name for a dynamic phenomenon that sometimes occurs during the launch and ascent of space vehicles powered by liquid propellant rocket engines.

The phenomenon is due to a coupling between the first longitudinal resonance of the vehicle and the fuel flow to the rocket engines.

VibrationdataVibrationdata

9

Gemini Program Titan II Pogo

Astronaut Michael Collins wrote:

The first stage of the Titan II vibrated longitudinally, so that someone riding on it would be bounced up and down as if on a pogo stick. The vibration was at a relatively high frequency, about 11 cycles per second, with an amplitude of plus or minus 5 Gs in the worst case.

VibrationdataVibrationdata

10

Flight Anomaly VibrationdataVibrationdata

The flight accelerometer data was measured on a launch vehicle which shall remain anonymous.  This was due to an oscillating thrust vector control (TVC) system during the burn-out of a solid rocket motor.  This created a “tail wags dog” effect.  The resulting vibration occurred throughout much of the vehicle. The oscillation frequency was 12.5 Hz with a harmonic at 37.5 Hz.

-4

-3

-2

-1

0

1

2

3

4

87.0 87.5 88.0 88.5 89.0 89.5 90.0 90.5 91.0 91.5 92.0 92.5

TIME (SEC)

AC

CE

L (

G)

LAUNCH VEHICLECONTROL SYSTEM OSCILLATION AT STAGE 1 BURN-OUT

11

Flight Accelerometer Data

-10

-5

5

10

0

44.35 44.36 44.37 44.38

DOMINANT FREQUENCY = 1600 Hz

TIME (SEC)

AC

CE

L (

G)

MTTV6 RV X-AXIS GAS GENERATOR OSCILLATION1000 Hz to 2000 Hz

VibrationdataVibrationdata

12

Sine Function Example VibrationdataVibrationdata

-1.0

-0.5

0

0.5

1.0

0 0.5 1.0 1.5 2.0

TIME (SEC)

AC

CE

L (

G)

13

Sine Function Bathtub Histogram VibrationdataVibrationdata

-1.5 -1 -0.5 0 0.5 1 1.50

200

400

600

800

1000

1200

1400

1600

1800

2000 Histogram

Co

un

ts

Amplitude

14

Sine Formulas

The acceleration a(t) is obtained by taking the derivative of the velocity.

Sine Displacement Function

The displacement x(t) is

where

X is the displacement ω is the frequency (radians/time)

The velocity v(t) is obtained by taking the derivative.

VibrationdataVibrationdata

x(t) = X sin (t)

v(t) = X cos (t)

a(t) = -2 X sin (t)

15

Peak Sine Values VibrationdataVibrationdata

Peak Values Referenced to Peak Displacement

Parameter Value

displacement X

velocity X

acceleration 2 X

Peak Values Referenced to Peak Acceleration

Parameter Value

acceleration A

velocity A/

displacement A/2

16

Acceleration Displacement Relationship VibrationdataVibrationdata

Shaker table test specifications typically have a lower frequency limit of 10 to 20 Hz to control displacement.

Freq (Hz)Displacement

(inches zero-to-peak)

0.1 9778

1 97.8

10 0.978

20 0.244

50 0.03911

100 9.78E-03

1000 9.78E-05

Displacement for 10 G sine Excitation

17

Sine Calculation Example

peaktozeroinch039.0peak

X

G2sec/in386G5.2

])Hz25(2[1

peakX

peakX1

peakX

2

2

What is the displacement corresponding to a 2.5 G, 25 Hz oscillation?

VibrationdataVibrationdata

18

Sine Amplitude VibrationdataVibrationdata

Sine vibration has the following relationships.

These equations do not apply to random vibration, however.

RMSX2peakX

peakXX2RMS

1

19

SDOF System Subjected to Base Excitation VibrationdataVibrationdata

20

Free Body Diagram VibrationdataVibrationdata

Summation of forces in the vertical direction

Let z = x - y. The variable z is thus the relative displacement.

Substituting the relative displacement yields

)x(yk)xy(cxm

kzzc)yzm(

ymkzzczm

y(k/m)zz(c/m)z

xmF

21

Equation of Motion VibrationdataVibrationdata

By convention,

nωξ 2c/m

2nωk/m

yz2nωznω2ξz

Substituting the convention terms into equation,

is the natural frequency (rad/sec)

is the damping ratio

This is a second-order, linear, non-homogenous, ordinary differential equation with constant coefficients.

22

Equation of Motion (cont) VibrationdataVibrationdata

yz2nωznω2ξz

Solve for the relative displacement z using Laplace transforms.

Then, the absolute acceleration is

yzx

y could be a sine base acceleration or an arbitrary function

23

yz2nωznω2ξz

A convolution integral can be used for the case where the base input is arbitrary.

d)-t(sin)-t(nexp)(Y1

=)tz(t

0 dd

2nd 1

A unit impulse response function h(t) may be defined for this homogeneous case as

where

tsin)texp(1

=h(t) dnd

Equation of Motion (cont) VibrationdataVibrationdata

24

Equation of Motion (cont) VibrationdataVibrationdata

The convolution integral is numerically inefficient to solve in its equivalent digital-series form.

Instead, use…

Smallwood, ramp invariant, digital recursive filtering relationship!

25

Equation of Motion (cont) VibrationdataVibrationdata

2idnd

n

1idd

dn

idnd

2in

1idni

yTsinTexpT

1T2exp

yTsinT

1TcosTexp2

yTsinTexpT

11

xt2exp

xtcostexp2x

26

Sine Vibration Exercise 1VibrationdataVibrationdata

Use Matlab script: vibrationdata.m

Miscellaneous Functions > Generate Signal > Begin Miscellaneous Analysis >

Select Signal > sine

Amplitude = 1

Duration = 5 sec

Frequency = 10 Hz

Phase = 0 deg

Sample Rate = 8000 Hz

Save Signal to Matlab Workspace > Output Array Name > sine_data > Save

sine_data will be used in next exercise. So keep vibrationdata opened.

27

Sine Vibration Exercise 2 VibrationdataVibrationdata

Use Matlab script: vibrationdata.m

Must have sine_data available in Matlab workspace from previous exercise.

Select Analysis > Statistics > Begin Signal Analysis >

Input Array Name > sine_data > Calculate

Check Results.

RMS^2 = mean^2 + std dev^2

Kurtosis = 1.5 for pure sine vibration

Crest Factor = peak/ (std dev)

Histogram is a bathtub curve.

Experiment with different number of histogram bars.

.

28

Sine Vibration Exercise 3 VibrationdataVibrationdata

Use Matlab script: vibrationdata.m

Must have sine data available in Matlab workspace from previous exercise.

Apply sine as 1 G, 10 Hz base acceleration to SDOF system with (fn=10 Hz, Q=10). Calculate response.

Use Smallwood algorithm (although exact solution could be obtained via Laplace transforms).

Vibrationdata > Time History > Acceleration > Select Analysis > SDOF Response to Base Input

This example is resonant excitation because base excitation and natural frequencies are the same!

29

Sine Vibration Exercise 4 VibrationdataVibrationdata

File channel.txt is an acceleration time history that was measured during a test of an aluminum channel beam. The beam was excited by an impulse hammer to measure the damping.

The damping was less than 1% so the signal has only a slight decay.

Use script: sinefind.m to find the two dominant natural frequencies.

Enter time limits: 9.5 to 9.6 seconds

Enter: 10000 trials, 2 frequencies

Select strategy: 2 for automatically estimate frequencies from FFT & zero-crossings

Results should be 583 & 691 Hz (rounded-off)

The difference is about 110 Hz. This is a beat frequency effect. It represents the low-frequency amplitude modulation in the measured time history.

30

Sine Vibration Exercise 5 VibrationdataVibrationdata

Astronaut Michael Collins wrote:

The first stage of the Titan II vibrated longitudinally, so that someone riding on it would be bounced up and down as if on a pogo stick. The vibration was at a relatively high frequency, about 11 cycles per second, with an amplitude of plus or minus 5 Gs in the worst case.

What was the corresponding displacement?

Perform hand calculation.

Then check via:

Matlab script > vibrationdata > Miscellaneous Functions > Amplitude Conversion Utilities > Steady-state Sine Amplitude

31

Sine Vibration Exercise 6 VibrationdataVibrationdata

A certain shaker table has a displacement limit of 2 inch peak-to-peak.

What is the maximum acceleration at 10 Hz?

Perform hand-calculation.

Then check with script:

vibrationdata > Miscellaneous Functions > Amplitude Conversion Utilities >

Steady-state Sine Amplitude

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