:aofiuhl - dticin azimuth. the received cignal is assumed to be due to at most two point sources. it...
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C) TliE RESÜLVABILITY OF PODTT SOURCES'
Peter Swer'J iru; Sn>^lneerinß Division The RAOT Corporation
P-l '2
Deceaber ö, 19">9
COPV
w%y i/i w\:aoFiuhL
f*! .J U k.
i i
To be presented -i* the o/uiposiu:;: or: Decibio;. T-.eorj at Ko-,e Air Development Cer:ter, May 1)0.
r h r P A N D C ü r p o ' a • i o n • 5 n n I a M a " i t a • C o I ■ f o f n i ti
Fho views e.'picssed in this paper are not npressrinly ttioso of the Corporation
r Lb
- ^,7
, -,'- r p .
D)rÖ)^^Pr-^rn: M »if
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·•·
THIS DOCUMENT IS BEST QUALITY AVAILABLE. THE COPY
FURNISHED TO DTIC CONTAINED
A SIGNIFICANT NUMBER OF PAGES _WHICH . DO NOT
REPRODUCE LEGIBLY.
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P-l ■ 2 li
SUMMARY
The probler, invcGtigated is the resolvability, in the presence of noise,
of point so'drces vhich are Gepturated In aziruuth by less than the width of
the main lobe of the gain pattern.
The probability of correctly resolving two sources is derived for a
particular class of decision methods as a function of the strengths of the
sources, their angular separation and noise level. Numerical results are
presented for a case which corresponds :;iore accurately to optical or infra-
red aevices than to redar.
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1
I. INTRODUCTION
The question of resolvability of point targeto, or point sources, arises
in radar, infrared, and optical applications.
First let us distinguish the problem of resolution from that of accuracy.
The accuracy probleir. is concerned with the errors in determining the position
(l 2) of an isolated source. It is, for example, well known ' that the error
in determining angular position of a radar target iray be much less than the
width of the main lobe of the antenna beam.
The word "resolution" covers several related concepts. In photography
or radar ground mapping, resolution has to do with the quality in some sense
of the picture, or with the ability to pick out certain features of the
picture. On the other hand, the type of resolution with which we shall
here be concerned is the following: suppose the received signal is known
to be due to a relatively small number of point sources; resolution consists
in deciding exactly how many sources are actually there. We will also limit
the discussion to angular resolution; resolution in range or range rate will
not be considered=
A widely used rule of thumb is that point sources are resolvable If
they are separated by (roughly) at least the width of the main lobe of the
gain pattern. (By gain pattern is meant, in radar applications, the antenna
gain pattern; in infrared or optical applications, the intensity pattern of
the image of a point source. ) While this is a useful rule of thumb, it
falls to answer many important questions. This can be illustrated by the
fact that, in the absence of all noise, and if the gain pattern were per-
fectly known, it would in many cases be possible to make error-free decisions
as to the number of sources regardless of their relative positions or strengths,
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P-lc.2 2
A re solvability criterion should therefore involve the probabilities
of making correct decisions as to the number of sources present, and the
manner in which these probabilities depend on the noise level, on the strengths
and positions of the sources, and on the gain pattern.
Ideally, the criterion should reflect the intrinsic dependence of re-
solvability on these factors, where by "intrinsic" is meant the (in some
sense) irreducible dependence, apart from the particular decision method
employed. However, due to difficulties in arriving at a satisfactory treat-
ment of "intrinsic" resolvability, the approach to be used here Is based on
analysis of the performance of a particular class of decision methods.
It is clear that the resolution problem as defined above is a problem
of statistical hypothesir testing. However, the problem of finding an
optimum test cannot be answered by the Neyman-Pearson likelihood ratio test,
since, if the problem is not to be simplified out of existence, the positions
and strengths of the sources must be regarded aa not known a priori. Thus,
the problem is one of testing composite hypotheses against composite alter-
natives, leading to all the well-known difficulties of defining optimum
tests in-situations of this type.
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*. ~ -L . u
:5
II. A CLASS OF RESOLUTION DECISION METHODS
It will be a.-.sumed. that we are dealing with a detection device scanning
in azimuth. The received cignal is assumed to be due to at most two point
sources. It will be assumed that the output of the detection device is
sampled at a series of angular positions x., i » 1, •••, K, resulting in the
presentation to a decision-making device of a series of magnitudes v., 1=1,
•••, K. (If we eure dealing with a pulsed radar, this sampling occurs auto-
matically; otherwise, such a sampling may always be defined to be part of
the decision procedures which are to be considered.)
It will be supposed that, when two sources are present, one can repre-
sent v by
v, i c^ FU. -■ \) + ti2 F(x. " "^ ^ V (1)
Here QL and Q are equivalent to the strength of sources located at angular
positions T and x ; F(x ) represents the gain pattern; and n is the noise
component of v.. The single-source case may be obtained by putting eithor
O, " 0, a = 0 or i, a t . (Not all physical situations can be represented
by Eq. 1; more will be said about this below. ) a
The following assumptions will be made regarding F and n.:
(a) F is a known function. Thus, attention is focusaed on tre limitations
on resolvability due to noise; that due to imperfect knowledge of the gain
pattern is ignored.
(b ) The gain pattern F is assumed to be a non-negative, even function.
(c) The range of observations v., i = 1. ••■, K, the gain pattern F, the
possible source positions T and the density of observations are such that,
to goci approximation.
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P-lb£2
K K S F(xj - T) - y~^ F(x,) - 3, all T (c)
1 = 1 1*1
K y" F(x, - T] F(xi - T2) - P(T1 - T2) = p(-l-2 - T1) (5)
(d) The noise components n^ have knovn means n. (hpnce, the means are inde-
pendent of the unknown parametere CL , a0, T , T0). Thus, it is no loss of
generality to aesume that
n = 0; all i (U)
It will not, however, be asEumed that the higher order n-ionente of n, are
necessarily independent of a , a , -r^ , T0. 1. ti L c
(e) The noises n. Bind n, are statistically independent for i ^ J.
These asauaptionü, incidentally^ simplify many of the mathematical ex-
presBions but are not really eßsential to the basic approach.
Now, define
K
v - - y v (5) 1 B 4-T- i KJ,
i=l
K
>w ^r Vl'
Observe that, if n. = 0, all i, then
0(T - T )"] V/ - V,, « 2a.ap 1 i ^- (7)
^ 2 L p(0) j
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p-ie62 5
A reasonable decision nethod would therefore be to announce two sources
or one source according to whether V is greater or less than a pre-assigned
threshold. Observe that, if n » 0, all i, then V is zero if, and only if,
either O. ■ 0, a ■ 0, or T « T .
It iums out, however, that this decision niethod must be modified in
most cases of interest, for the following reason: if n ^0, then (denoting
expected values by bars )
K
1 1 2 V - V » 2a a vl 2 12
1 ± i_
p(0) J i 2
B p (0)J i-1 n. (8)
2'
' 2 In some interesting cases, the quantities n. depend on OL and a0.
/vlso, the higher moments of V as defined by Ej.. (?) niay depend on OL and a
even if the statistics of n, do not.
The class of decision methods to be analyzed can be defined as follows:
announcement of two sources or one source according to whether V is cheater
to or less than a pre-assigned threshold, where V is some function of V and
V0. The specific form of V will depend on the manner in which the moments
of n. depend on OL , a , T,, and T„, in the particular case under considerati
It is clear that all necessary information about the performance of
this class of decision procedures can be deduced from the Joint probability
density of V1 and V^.
on,
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P-1562
III. THE JOIM1 PROBABILITY DENSITY OF V AKD V
It will now be assumed that the nui.-.ber K of observations is sufficiently
great so that both V. and V are norrÄl randorr. variables (within the range
of probabilities which we wish to compute). Thus, the Joint density of
V and V will be completely specified if one can compute V , V , V , V ,
and V V , or the equivalent. Computation of chese quantities ia a straight-
forward process. The results are,
V ■» a + Q 1 1 2 (9)
-lO
LV1J
K
B . i«l / n. (10)
2 2a
1Q2 P^i " T2^
K 1 \ ' —;
V\ - a/" + a.;" + —^—— — + — I , n^ 1
)(0) p(0) i=l (11)
and, vritir.g for convenience
^ - o^ ^(x^^ - T1) + a^ F(xi - Tg), (12)
K
(0) i»l ^ : ' i i 2/^« ', ■■-' i i
D£'(0) i-1 (13)
1
r (o) i-i n.
viv2
v'iv2
J
BTTO]
K \ • p
2 / n. S. c ' i i i-1
K
i»l j (IM
This, of course, does not imply that V is norraal.
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P-lK'S
7
IV. RESULTS FOR A PARTICULAR CASE
In order to proceed further it is necessary to make definite assumptions
ais to the moments of n , which depend on the particular detection device
under consideration.
As an illustrative case, it vill be assumed that
ni
2 ni
3 ni
T ni
(15)
This (with suitable nonaalization ) would be the case if the n. were Gaussian
with means and standard deviations independent of a. , Q0. T., and T_. This
might describe some infrared or optical detection devices; it is not so easy
to +link of radar cases which would be adequately described in this manner.
The first and second order moments of V and V for this case can be
obtained by inserting (l^) into (9) - (l^)j the results need not be written
out in detail. It turns out that
2,^ K[B - p(0)] , 1 2 B p(0) ^ c
Pt^ - T2) 1 RöT" (16)
An appropriate resolution test is defined by V > threshold, where
V . i (V 2 v KjB^Mll . (17) Vl I 1 2 B2 p(0) J
Note that in the absence of noise, one would have
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p(T1 - T ) 1 - ~ ~
P(O)
I-X::i2 8
(16)
Even with all the special assumptions which have thus far been made,
it would still be possible to generate numerical results ad inTinltura.
Therefore, numerical results will be shown only for the following special
case:
Let 2
r(x) - e"X (19)
1 1+1 1 20
(20)
Then, approximately.
B - 20 xHT (21)
p(T1 - T2) - 20 j~|~ exp L | (^ - T2)2j (22^
The range of observation will be chosen from x - -2 to x « +2. With
this choice of observation range, K ^ 50. The choice of observation range
ought really to be the solution of an optimization problem. However, the
choice is here somewhat restricted by the requirement that the sums in Eq's.
(2) and (3) should satisfy Eq's. (2) and (o) to good approximation, for all
values of T and x under consideration. We will be interested in values
of 1^ - T up to about 1.5, and the range x ■ -2 to x • +2 was chosen as,
roughly, the smallest range for which (2) and (i) would hold for all values
of T^ - T up to 1.5.
The results obtained foi this case will clearly also apply to any case
of the form:
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P{x) = exi (' 1~' ) ' coservation ran^e x n -2;- to x » +2D; x, -i " ;,: = ~r'
and all i /aluec multiplied by l:.
All ;;arar„eter vulje,. will be chosen :;c t-hat, the prcbability o:' fall'are
tu detect any source at all !s i.efjl ;,■;. i'io.
Figureo L-10 bhow probability d-str; but Ion -/unctions for V (as defined
by (I?)) for a variety of 7alueü of u , u,,, and T - T.,. In these figurea,
Pm - ProV- (V T) (2.0
One ;;..;.;ht dej.re LL proben' this ;;.:'..rrr.ation in alternative :\:;:.;. An
illustration of thiü .c r.-'-e-'. in Fns. 11-1.'.
Define
P [twc I Ot . u , T - T,,] (21. )
» probability of correctly anncmci:^
two sources, .: t).e;-e are in realit;«
two sources ci'.arHCterized ny tne
ara-T.eters .1. . ;_, 1, , T . i c i 2
Also, let
P[t.wo 1-^, 0] (25)
= probability cf falsely anncuncing two
sources, if in reeuity only one soui'ce is
prebent character''zed by the parameter ct .
Frei:. Fig. 1, we ■ ee trat ■ r. tlie 1 resent ca^c, P[ two I '^ ; C] is nearly independent
of ■« n . provided t:.',.s probabil^t', :s relativelv j::.nll. L
Figures li, IT, ar.d !.• show P[two I /. , ü,., i, - T0] subject to the con- 1 C 1 it
iition P[two 1 30, G; = .10.
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10
It ran also he verified .'n the particolar raue ander consideration that
•esolution perTorrr-ance, when rresented in the i'or::. of curveB like those of
"if'u, -.1-1', rer:.a;n5 roiu-'hiy ti.e aai.-.e if x . - x., Q and rj.„ a-e all
::ulti]lLed iij the jo.,.e 1'actor (other ijararneterü renyiining unaltered).
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11
V. ADDITIONAL TOPTCS FOR INVE3TIGAT:ON
Come additional topics which woula Le i-sel'.il tc investigate are >-^
f'ollovs:
i. Investigation of cuces 1;J w;., •;. f.-.e '.or.' .A.^ cf n. (oti.er than the
l'irüt) depend D.I x , Ci,,, T , and T0. TIILü wo'ild include some radar caües;
for exa;-iple :
(a) Noise-like taryetü (or noise 'aj.jr.ln^) detected b^ a radar.
In this caae, the output of a square lav envelope detector, properly norral
ized, would have probability density function
exp 1 + 07 F(x. - Tp + a F(x^ - 7,jj ,(v ) . h i 1 i : : 1- (:()
1 + a. F(x. - •:. )>.'... r(x. - TJ 1. A L tic
(b ) Non-fluci.uating targets, the relative phase of one target
return with respect to the other varying randorily i'rot;. pulse to pulse.
One would expect that in these cases the resolvabillty of targets
separated by less than a bearawidth would be seriously degraded aa compared
with the case considered in the previous section.
2. Dropping the requirement that F b§ an even function and always
positive. This might be of interest in analyzing a scanning monopulse radar,
Here it might be necest-ary to use functions of the data ether than V and V ,
Dropping the requirement that n.n » 0 for i / .i.
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?-L-y6c
1
t
■J 1
( 1 w
0 20
0 IC
0 05
0 02
00i
0 005
0 00?
0 001
1 . L.
F,g
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1-5
0 999
0 99B
0 99
0 9B
09b
0 90
0 80
0 70
0 60
0 50
0 40
0 '■■)
0?0
0 10
0 0b
002
OOi
0 00 b
0 002
0 001
a ,
-1
4
A
0 T
Fig 2
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0 999
0998
0 99
098
095
0 90
080
0 70
060
0 50
0 40
0 30
3 20
010
0 05
00?
0 01
0005
0002
0001
a
r, - r, = 0 i
1
0 T
Fig 3
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15
0 499
0 39B
099
098
0 9L;
090
0 80
0 70
0 60
0 50
0 40
0 30
0 20
0 :0
QL^
002
00i
0 005
000?
0001
T r,
0 f,
0 9
i 2
i 5
10
"1
-1
0 T
Fig 4
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io
0 999
0 99B
0 99
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0 9 b
0 90
080
0 70
0 6 0
0 ri0
0 40
0 ^0
0 20
0 10
0 0 5
0 0?
0 01
0 005
0 002
0 00 i
r, r? o
^' ^
0 6
0 8
J
A
0 T
Fig 5
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0 999
0 998 i
i
10
10
0 99
0 9'
OO'b
0 90 -
0 80 -
0 70 ■
0 60 -
050
0 40 -
0 30
0 20
0 iO
U05
0 02
OO1
0 005
0 00 2
0001
r, - 7. 0 2
0 3
0 .1
0 5
H
"1
0 1
Fig 6
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p-1862 18
Li ^S
r. uQ
0 RO
ü ^0
C hC
0 50
0 40
0 '.0
0 20
0 i0
005
002
001
000b
0002
0001
0 5
0 6
C 9
2
A
0 T
Fig 7
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r P-1562
19
f"j 99
0 98
0 95
0 90
0 BO
0 '0
0 60
0 50
0 40 -
0 30 -
0 20 -
0 10 -
005 -
002 -
OOl -
0 005 -
0002
OOOi
a a
50 3
0 2
0 4
06-
0 8
-? 0
Fig 8
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0 50
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0 5
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Fig 9
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P-lSö.
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0.
K ,'
10
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REFKKENCtS
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Swe:-l r.. ,
, "Maxi.:.'. - A;.(.;,J;u- Ace ,-'";,,• •'•>••, no. ', Gerjt.e;:.^sr i '■ ' .
a FulG'.'d Searci". Radar," Proc
Pernsr.cn, R., "A:i Anaiysiu or An-A a: Acc.;rp.cy i;: liearch Ruir.r/' l/^:,- L.R.E. Cor.vent^on Record, K'.rt ;, :• . ■'- ' .