Pre-Phase A Report - Lisa - Nasa
Pre-Phase A Report - Lisa - Nasa
Pre-Phase A Report - Lisa - Nasa
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100 Chapter 4 Measurement Sensitivity<br />
4.3 Signal extraction<br />
4.3.1 <strong>Phase</strong> measurement<br />
Information is extracted from the beat signal as a time series of phase measurements. The<br />
phase of the beat signal between the received and transmitted beams is measured with<br />
the time base provided by the on-board USO in each of the spacecraft. The two laser<br />
beams being beat together have different frequencies because of gradual changes in arm<br />
length and because of the roughly 10 kHz offset frequencies used in the locking scheme.<br />
The expected Doppler shifts for arms 1 and 2 (see Sections 3.1.1 and 3.1.2 and Figure 3.1)<br />
are of the order of 1 MHz for annual orbit corrections, and could be kept below 20 kHz if<br />
necessary by monthly orbit corrections. For arm 3, the Doppler shifts may be as high as<br />
15 MHz.<br />
The phase of the laser heterodyne signals needs to be measured with an accuracy much<br />
better than the total error allocation of 40 pm/ √ Hz and with a dynamic range of roughly<br />
109 in order to perform the laser phase noise cancellation scheme. Forty picometers<br />
corresponds to 4×10−5 of a cycle, and the expected laser phase noise was estimated earlier<br />
to be roughly 30 Hz/ √ Hz at 1 mHz (see Section 3.1.5). This corresponds to roughly<br />
3000 cy/ √ Hz for the phase noise at 1 mHz . In order to measure the phase to the necessary<br />
accuracy and with the desired dynamic range, the signal from each optical heterodyne<br />
detector is beat again against a suitable reference frequency from a comb of frequencies<br />
separated by intervals of 50 kHz, which are generated from the USO. The reference frequencies<br />
are chosen to place the final beat frequencies in the range of 75 to 125 kHz. A<br />
tracking filter is then used to remove phase noise above roughly 100 Hz in order to prevent<br />
aliasing of such noise into the phase measurements.<br />
The resulting signals are then sent to the phase meters, where they are strongly amplified,<br />
clipped, differentiated, and clipped again to give positive-going zero-crossing pulses with<br />
standard shapes. In each measurement interval, the delay between the USO clock pulse<br />
defining the interval start and the next zero-crossing pulse is timed, and the total number<br />
of zero-crossing pulses is counted. From this information the integer and fractional<br />
numbers of zero crossings are determined for each interval. The results are then filtered<br />
to remove phase variations at frequencies above about 1 Hz, and the data set is reduced<br />
to a time delay and a count every 0.5 s.<br />
4.3.2 Laser noise<br />
The data are affected by the phase noise of the master laser in S/C 1, as well as orbital<br />
motions and gravitational waves affecting the long arms. However, the variations in the<br />
arm lengths in the frequency band of interest, roughly 0.1 mHz to 1 Hz, are small. Thus<br />
the apparent variations in the length of any of the arms can be analyzed to determine the<br />
laser phase noise as a function of time. For simplicity only arms 1 and 2 will be discussed<br />
here, but similar results can be obtained for observables that include arm 3 also.<br />
The accuracy of the phase noise measurements will be degraded near harmonics of the<br />
frequencies corresponding to the round-trip travel times for the two arms. A weighted<br />
mean of the results for the two arms can be used to avoid this problem, but we assume<br />
3-3-1999 9:33 Corrected version 2.08