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Innovative SETIby the KLTClaudio Maccone
Member of INAF & Int. Academy of Astronautics
E-mail: [email protected]
Home page: http://www.maccone.com/
Astrophysics in the LOFAR era
Emmen (The Netherlands) 23-25 April 2007
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What is SETI ?
SETI is the Search for ExtraterrestrialIntelligence.
SETI began in 1960 with Project Ozmaconducted by Frank Drake.
No ET signal was found so far, but we only
explored distances < 100 pc.
The simplest form of SETI is to look for an alienCARRIER on a very narrow band (< 1 Hz)
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5 Complexity Levels for SETI
Level 1: Piggyback SETI at 1.420 GHz by FFT.
Level 2: Wideband SETI by KLT (LOFAR ?).
Level 3: Targeted Searches (on HabCat stars).
Level 4: Leakage Searches (by SKA
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SETI at Medicina (Italy)
The signal processing for SETI at Medicina is performedby an analyzer (Serendip IV) with a resolution of 0.6 Hz.
This spectrometer works with 24 million channels and a
15 MHz input bandwidth centered around the hydrogenline at 1.420 GHz, as traditional in SETI since 1960.
New post-processing algorithms have been successfullytested: the Hough transform for the Doppler effect
recognition (i.e. to cope for drifting signals) and
The Karhunen-Love Transform (KLT) to filter veryweak signals out of any colored background noise.
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From SETI to ASTEROIDAL RADAR at Medicina.
The SETI facilities at Medicina were first used in 2001 toDetect Space Debris and TEST the Asteroidal RADAR.
Ukraine (Crimea): Evpatoria 70 meter dish
Etalon 1, launched in 1989 (Laser ranging),orbiting at 19.000 Km
1.4 mt
Medicina:32 meter dish
S IVBW=15 MHzNch=24 M
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Di Martino, Montebugnoliet Al. 2004 paper
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MSPEC0: programmed for500 KHz @8192 channel15 Hz resolution (Real Time)
The minimal radar cross section min, which could be detectable with this Evpatoria Medicinasystem in GEO orbit can be estimated withmin = 4 r1
2 r222ks(S/N)min /PtStSrt
let r1=r2 =36.000 St=2500 m2 Sr=500 m2 =6 cm Pt=150 KW (S/N)min=10 t=10 sec
SETI back-end used for debris detection: so good that IT WENT OFF SCALE!!!
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2007 paper on KLT+SETI forasteroid & space debris RADAR
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Radar RANGE vs. S/N
4 S/N
1
S/N
1ERadar_RANG =
0.5 1 1.5 2 2.5 3 3.5 4 4.5 5 5.5 6 6.5 7 7.5 8 8.5 9 9.5 1030
54
78
102
126RANGE vs. S/N
S/N at Medicina IMPROVED BY THE KLT
RADARRANGEinthousandsofkm
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What is the KLT ?
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Example (a Newtonian analogy):consider a solid object, like a BOOK,described by its INERTIA MATRIX.
Then there exist only one specialreference frame where the InertiaMatrix is DIAGONAL. This is thereference frame spanned by theEIGENVECTORS of the Inertiamatrix.
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Newtonian Analogyto the KLT
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If two of the body dimensions are smallthen the corresponding moments ofinertia are very small too.
Thus, they are almost ZEROS in the
INERTIA MATRIX.And only the FIRST EIGENVALUE inthe Inertia Matrix is non-zero.
This is called DOMINANT eigenvalue.
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If is a stochastic process (= input to the radiotelescope) it can be expanded into an infinite series
then are orthonormalized time functions:
are random variables, not changing in time, withthe property
In conclusion, the KLT separates theradiotelescope input (= noise + signal(s))
intoUNCORRELATED
components.
KLT mathematics
( )tX
( ) ( )
=
=1n
nn tZtX Tt0
( )tn
( ) ( ) =T
mnnm dttt0
nZ
mnnnm ZZ =
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KLT mathematics
( ) ( ) ( ) ( )20
1121 tdtttXtX nn
T
n =Integral equation yielding both the Karhunen-Loveseigenfunctions and corresponding eigenvalues .
The kernel of this integral equation is the autocorrelation.
This is the best basis in the Hilbert space describing the(signal+noise). The KLT adapts itself to the shape of the
radiotelescope input (signal+noise) by adopting, as a referenceframe, the one spanned by the eigenfunctions of theautocorrelation. And this is turns out to be just a LINEARtransformation of coordinates in the Hilbert space. Thus, it is aneasily INVERTIBLE TRANSFORMATION.
( )tn n
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KLT filtering
There is no degeneracy (i.e. each eigenvaluecorresponds to just one eigenfuction only).
The eigenvalues turn out to be the variances of therandom variables , that is
Since we can SORT in descending order ofmagnitude the eigenvalues and the correspondingeigenfunctions. Then, if we decide to consider only the
first few eigenfunctions as the bulk of the signal, and toapply the inverse KLT, thats what KLT filtering is: we justdeclare the taken-off part as noise!
The Galileo mission by NASA-JPL used the KLT
nZ .022 >== nnZ Zn
0=nZ
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KLT vs. FFT
FTKLT
Fast algorithm FFTNeeds high computationalburden: no fast KLT
Is plagued by thewindowing problemsIs defined for any finitetime interval
Works OK for stationaryinput stochastic processesonly
Works for both stationaryand non-stationary inputstochastic processes
Rigorously true for narrowband signals only
Works well for both wideand narrow band signals
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Future SETI by the SKA
Table taken from the 2004
paper The Cradle of Life,
by Joe Lazio, Jill Tarterand David James Wilner,
New Astronomy Reviews,
Vol. 48 (2004), p. 985.
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Conclusions
SETI, the Search for ExtraTerrestrial Intelligence, has so farbeen investigated since 1960 only modestly by the internationalastronomical community. NASA was FORBIDDEN to do SETIby the US Congress in 1993. Some countries are doing poor
SETI today: USA, Australia, Argentina, Italy, Japan, France...This may be due to FEARS by the politicians that a contactwith ETs would shake the beliefs of Humanity too much...
The International Academy of Astronautics (Jill Tarter et Al.)issued SETI PROTOCOLS for ethical behavior in a Contact.
Lofar &SKA will enable much more refined SETI searches.
Its high time to EXPAND THE SETI SEARCHES
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Thanks !