THE EFFECT OF FORWARD MOTION COMPENSATIDN (FMC) ON RESOLVING POWER OF AERIAL PHOTOGRAPHS J. Hakkarainen, University of Joensuu, Finland M. Schroeder, DFVLR, FR Germany Abstract: Test flights with aerial survey cameras equipped with Forward Motion Compensation were carried out in May 1987 in Finland. To determine the resolving power a bar test pattern with low, medium and high contrast was used. Different film types were tested and the camera was operated with FMC on and off. The scale of the photographs was approx. 1 : 10 000. This paper presents the test results for a camera of 150 mm focal length .. 1. Introduction In May 1987 a test flight campaign was carried out at Nummela airfield (West of Helsinki) to determine the resolving power of various combinations of Aerial Survey Cameras and Aerial Films. In particular the effect of Forward Motion Compensation on resolving power should be investigated. The following cameras and films were used: Cameras: RMK A 15/23, RMK A 30/23, RMK A 8.5/23 Films: Panatomic-X, Plus-X, Double-X, CIR-2443, SO-131, SO-242 .. The cameras were operated in a two engine turboprop aircraft of the type Do 228/100 in an unpressurized cabin. The aircraft and the cameras were provided by the German Aerospace Research Establishment (DFVLR). To determine the resolving power aerial photographs were taken over a resolution test field on the ground. This test field was produced by J. Hakkarainen, University of Joensuu. The films were developed at the photo lab of the National Board of Survey and Topographic Service, Helsinki. In this report only results for the RMK A 15/23 camera will be presented. 2. The Test Field A sketch of the test field used to determine the resolving power is shown in Fig. 1. The test field was produced of 30 hard board plates, which were painted with mat paint. It also comprised a 6-step grey wedge for controlling the film development. 1... 1 At an image scale of 1 : 10 000 the spatial frequencies of the bar test pattern corresponded to 20, 30, 40, 50, 60, 70 and 80 lp/rnrn which were arranged in five parallel rows each with a different contrast. The test field was composed of two identical sets of these bar test pattern arranged perpendicular to each other. The various contrasts of the bar test pattern are given in Table 1. In this report not all contrasts have been used for data evaluation; for the black/white films only 1 : 20, 1 : 3 and 5 : 1 contrasts have been applied and the colour films only the 1 : 20, 1 : 3 and green/red contrasts. No. Background Density Bars Density Contrast Density Difference Ratio Remarks 1 black 1.60 white 0.30 1 .. 30 1 high contrast 2 grey 0.85 black 1 .. 60 0 .. 75 5 .. 5 3 grey 0.85 white 0.30 0 .. 55 1 3.5 low contrast 4 blue 0 .. 85 yellow 0 .. 15 0.70 1 5 colour contrast I 5 green 0.80 red 0.60 0 .. 20 1 1.5 colour contrast II Table 1: 20 1 shadow contrast Contrast ratios for the bar test pattern8 3. Test Flight Program Table 2 gives an overall view on the flights, which were carried out with the RMK A 15/23. The nominal flight altitude was 1530 m over ground to obtain an image scale of 1 : 10 000. Only for the flights with the 50-131 and 50-242 films the altitude was increased because a higher resolution than 80 lp/rnrn was expected. To image the test field at different look angles four consecutive overflights were made with an overlap of the photographs of 90 % and higher. The flight pattern which was applied for every flight series is shown in Fig. 2. 1... 1 Date Time Sun Elevation Altitude [m] over ground Film Fileer f-Stop I lit FMC No. of Images 28 14 Yes No 48 42 12 12 Yes No 14 Imaqe Motion [urn] 12.10-12.24 12.28-12.40 44· 45" 1530 1530 PAN X PAN X B B 5.6 I 250 12.44-12.54 12.55-12.59 45" 45" 1530 1530 DX DX B B 5.6 I 600 14.32-14.46 14.49-14.59 43" 42" 1530 1530 Plus-X Plus-x B B 5.6 I 450 16 16 Yes No 52 43 9 May 87 15.03-15.13 15.17-15.29 41" 40· 1530 1530 CIR-2443 B CIR-2443 B 5.6 I 250 5.6 I 350 28 20 Yes Yes 41 54 10 May 87 10.07-10.20 34" 2020 SO-131 KL 4.0 I 100 53 Yes 46 10 May 87 10.24-10.39 36" 2020 SO-242 KL 4.0 I 100 53 Yes 60 8 May 87 8 May 87 9 May 87 4.0 I 500 5.6 I 600 5.6 I 450 34 Table 2: Parameters of Test Flights with the RMK A 15/23. 4. Data Evaluation Method 4.1 Abreveations T-lines: bars of the test pattern perpendicular to the flight direction R-lines: bars of the test pattern parallel to the flight direction T: R: Resolution in lp/mm for the T-lines Resolution in lp/mu for the R-lines Average Resolution = AritlliTletric Mean of T and R ~T: Improvement in Resolution with FMC for T r: radial distance from the image center G/R: Green/Red-contrast 4.2 Determination of the Resolving Power (RP) The following criteria were used for determining RP: 1. A bar target ist accepted as resolved, if the nwTlber of lines is correct, all lines of the test figure are recognizable and not more than 20 % of the target is damaged . 2. A target ist not accepted as resolved, if the preceding target was not acceptable. 3. Visual interpolation is uSed between two targets, if the resolving power is obviously between these two targets. 1-1 1 For visual interpolation every interval of 10 lp/mm was subdivided in 4 sections of 2.5 lp/mm and the following rules were applied (e.g. for 30 and 40 lp/mm targets): 30 lp/mm 40 still acceptable clearly seen very clearly seen very clearly seen very clearly seen fully grey fully grey fully grey direction of lines seen still acceptable 30 .. 0 32.5 35.0 37.5 40.0 The determination of the RP was made from the original films by means of a binocular microscope with a 20 x magnification; only for the Panatomic-X and the SO-242 films the magnification was increased. Both authors made the observation indepently, Juhani Hakkarainen in June 87 in Joensuu, Finland and Manfred Schroeder in July 87 in Oberpfaffenhofen, FRG. Final RP values are average values of both observers. For those points for which the difference between the RP of the two observers was more than 25 % the RP was determined for a second time by both observers. Such cases were less than 5 % of all observations. For the controlled points 4 observations were then availablee The highest and lowest value were then dropped as a cross error control and the final RP was the average of the two center values. For scale control the image scale was determined by measuring the size of the test field in two images per test flight strip. A scale correction was needed only for few flights .. The RP values can be plotted as function of the radial distance; this is shown e.g. for the Plus-X film with FMC 'on' in Fig. 3 a. The dispersion of the RP points is considerable. For fitting a curve through these points the RP values were averaged for radial intervals of !:i r;:;; 25 mm; the average RP points were then connected resulting in the 'resolution curve' (Fig. 3 b). The standard deviation of the resolution curve is indicated in Fig. 3 c. 4.3 Area Weighted Average Resolution (AWAR) If R (r) is the resolution as function of the radial distance then the AWAR is given by AWAR = old R (r)· G (r) dr ; d = 162,6 mm G (r) is the Area Weighting Function and is given by: 1-172 = G (r) = and G (r) S = 21T ( e r for 0 < r < S F s 1T /2 - 2 arccos r) · r for S < r < d F/4 F: total area of photograph 115 rom = (230)2 rom 2 The AWAR was determined for T - and R-lines from the resolution curves (s. 4.2); the RP was determined graphically from this curves at distances of b. r = 15 rom. For numerical integration the following values for G(r)edr were used: r G( r) edr 0.027 0.053 0.080 15 rom 30 45 r G·dr r G-dr 60 75 90 0.107 0.134 0.160 105 120 145 0.187 0.142 0.100 For determination of the RP for r > 120 rom the resolution curves were graphically extrapolated is some cases. AWAR values will be given in the next section (5). 5. Resolving Power Results 5.1 Panatomic-X Film For the Panatomic-X film two flight series were carried out: one with FMC 'on' and the settings 5.6 - 1/250 and another with FMC 'off' at 4 - 1/500. The results are shown in Fig. 4. For all contrast the T-lines are better resolved with FMC 'on'. For the R-lines the resolution is better in the center (r < 50 rom) with FMC 'off', whereas it is the same for the other part of the image ( r > 50 rom). The difference in the center part can be explained by the shorter exposure time for the flights with FMC 'off', which minimize the influence of aircraft attitude movements. For the R-resolution the curves from the flights with FMC 'off' can be regarded as the more representative values. From the curves in Fig. 4 the following AWAR-values can be derived: FMC on Contrast 1 5 1 20 1 3 R T M FMC off T 60 lp/mm 43 50 65 51 55 63 47 53 53 39 47 1-173 b.T 23 % 31 % 17 % The T-resolution with FMC is always higher than the Rresolution. The improvement in T-resolution with FMC varies between 17 % and 31 %. Curves for the average resolution (with FMC) for different contrasts are shown in Fig. 5. 5.2 Plus-X Film Two flights series - one with FMC 'on' and one with FMC 'off' - were carried out with the Plus-X film. The exposure settings for both series were 5.6 - 1/450. The obtained resolution curves are shown in Fig. 6. For all contrasts the T-lines are better resolved with FMC 'on'. For the R-lines there is no difference in resolution between FMC 'on' and FMC 'off'. From the curves in Fig. 6 the following AWAR-values were derived: FMC on Contrast 1 5 1 20 1 3 R T M 39 lp/mm 25 42 27 32 34 41 26 33 FMC off T 36 25 30 !1T 17 % 8 % 13 % With FMC 'on' the T-resolution is slightly higher than the R-resolution, whereas with FMC 'off' R is slightly higher or equal T. The increase in T-resolution with FMC 'on' is between 8 and 17 %. 5.3 Double-X Film For the two flight series with the Double-X film - one with FMC 'on' and one with FMC 'off' - the exposure settings were 5.6 - 1/600. Due to the short exposure time the image motion, which had to be compensated for, was only 12 ~. The resolution curves for the T- and R-lines are shown in Fig. 7. For the FMC-off flights only 14 points were available to derive these resolution curves. For the T-lines the resolution for the FMC-on flights is slightly higher for all contrasts for radial distances r < 90 mm, wheras for r > 90 rom the resolution seems to be the same. For the R-lines there is no significant difference in resolution. From the curves in Fig. 7 the following AWAR-values were obtained: 1... 174 FMC on Contrast 1 20 5 1 3 1 R T M FMC off T 35 lp/mm 23 27 39 26 31 37 25 29 37 22 30 llT 5 % 18 % 3 % The gain in resolution for the T-lines can clearly be observed only for the 5 : 1 contrast. 5.4 CIR-2443 Film Two flight series with FMC 'on' were carried out for the CIR-2443 film with different exposure settings: 5.6 - 1/250 and 5.6 - 1/350. As no significant difference in resolution was observed for the two exposure times, the data sets from both flights were jointly evaluated. The results are shown in Fig. 8. The resolution for T- and R-lines are nearly the same, although T is always slightly higher than R. The following AWAR-values were derived from the curves in Fig. 8. Contrast 1 :: 20 1:: 3 G/R R T M 28 lp/mm 24 25 30 26 27 29 25 26 The resolution for the G/R-contrast is nearly the same as for the 1 :: 3 black and white contrast. 5.5 CIR - SO-131 Film The 50-131 film was flown with FMC 'on' and an exposure of 4 - 1/100. At this exposure time 53 ~ image motion had to be compensated for. The resolution curves are shown in Fig. 8. No distinct difference in resolution between Rand T can be observed. For determining the AWAR the curves in Fig. 8 were linearly extrapolated. The following AWAR-values were obtained: Contrast 1 : 20 1: 3 G/R R T M 33 lp/mm 28 33 34 28 34 34 28 34 The resolution for 1 : 20 black and white - and for the G/R-contrast is the same. For R- and T-lines resolutions between 50 and 60 lp/mm can be reached in the image center. 1. . 175 5.6 Colour 50-242 Film The 50-242 film was exposed with 4 - 1/100 and with FMC on. The image motion at this exposure time was 53 ~. The resolution curves are shown in Fig. 9. The T-lines are for all contrasts better resolved than the R-lines. For determining the AWAR the curves were linearly extrapolated and the following AWAR-values were obtained: Contrast 1 : 20 1: 3 G/R R T M 52 lp/mm 49 57 55 55 52 40 44 42 For the high contrast the T-lines reach over 80 lp/mm in the image center. There is only a slight difference in resolution between contrasts 1 : 20 and 1 : 3. 6. Conclusions o The FMC has only an effect on the lines perpendicular to the flight direction. o With FMC the resolution of the lines perpendicular to the flight direction (T) is always higher than for the lines parallel to the flight direction (R). Without FMC T is less or equal R. o The improvement in resolution perpendicular to the flight direction (T) can be as much as 30 % depending on the contrast. This effect is most pronounced for the PAN-X film, less pronounced for the Plus-X film and is relatively weak for the Double-X film. o Improvement of the AWAR for lines perpendicular to the flight direction (T) for the various contrasts: Film\Contrast 1 : 20 1 : 3 5 : 1 PAN-X Plus-X Double-X 23 % 17 % 17 31 13 5 % 3 8 18 o With the PAN-X film and the 50-242 film resolution values over 80 lp/mm can be obtained for high contrast in the central part of the image. 1. . 176 o The ranking of the films by AWAR-values is as follows: black/white-films PAN-X Plus-X Double-C 1 : 20 1 : 3 5 : 1 63 lp/mm 41 37 53 33 29 47 26 25 1 : 20 1 : 3 G/R 55 lp/mm 34 29 52 28 42 34 26 Colour-films SO-242 50-131 CIR-2443 25 Plots of the average resolution (M) for different film types for a contrast 1 : 3 are shown in Fig. 10. o The gain in resolution with the PAN-X film in comparison to the Plus-X and Double-X is between 50 and 80 % depending on the contrast. o With the Colour 50-242 film nearly the same resolution can be obtained as with the PAN-X film. o The gain in resolution with the SO-131 film in comparison to the CIR-2443 film is not as high as one would expect because of their difference in granularity. The reason for this is obviously that the resolution for ColourInfrared films is limited by the inadequate colour correction of the lens. o For exposure times longer than 1/300 sec it was often observed that also the lines in flight direction were partly deteriorated by pitch movements of the aircraft. References M. Schroeder, Auflosungstests mit ReihenmeBkammern aus groBer Flughohe. Proceedings of the 37th Photogrammetric Week, Stuttgart 24.-28.09.1979. J. Hakkarainen, Resolving Power of Aerial Photographs, Surveying Science in Finland, Vol. 4, No.2, Nov. 1986. 1... 177 Fig. 1: ratios@ 50, bU, details Test field with bar targets of different contrast The spatial frequencies correspond to 20, 30, 40, 70 and 80 lp/mm for a 1 10 000 scale. For more refer to Table 1. r-:=~ I (I I I I" : I I I I : I : '--. I ____ ~ I A 1-+-------11----__'.- +, I I I ~ I "- - . . - l - I - - - - - l - - - - - l - - - l" ~ I +- - ---+ END )l -- - - 1- - - - - - -..., I I I Fig. 2: Flight pattern for recording the test field on consecutive image frames during four overflights. 100 PAN-X 90 a ~ ...J o (J) 50 40 30 lJJ n::: 20 10 00000 N m ..q- IJ1 RADIAL DISTANCECmm) Fig. 5: Average Resolution (M) of PJ~K A 15/23 with Panatomic-X film for the contrast ratios 1 : 20, 1 5 1. 1. . 1 3 and ;~[J.J 100 PLUS-X PLUS-X 90 90 80 EE 80 EE 70 "-0... :: 60 a) 15 50 ~ ..J o Ul W 0:: 70 "-0... o § 0 0 o 0000 0 o 0 [JDO 0 0 0 o lb 40 8 60 15 50 ~ o '* 40 ..J 30 ** '* *:'Jf* ~ * * * ... '* ** ** <II- '* "\. ** 30 Ul W 0:: 20 20 10 10 ",1""1""1""1""1""1,,,,1,,,,1,,,,1,,,,1,,,,1"!,I",,I o '" o m o " o lfJ o ~ a ~ 0 00 0 rn 0 0 0 0 N 0 m a ~ o o lfJ " RADIAL DISTANCE(mm) . __ ._..l_.-,...~O R PLUS-X 100 70 EE 8 60 0... ~ 60 15 50 15 40 ~ ..J o 30 Ul W 0:: 20 a 0 .. ___ ._._~, m 0 tn '<t 50 40 30 10 o o m o " o lfJ o (j) a ~ a 00 a rn 0 0 a a N o m RADIAL DISTANCE(mm) o " o lfJ RADIAL DISTANCE(mm) .___...L.'--ZQ_R ... PLUS-X 100 .LL .._~" ..... L 100 ..•.•. _._ ... __ . .•_ _ ._. . ._ PLUS-X 90 90 80 80 EE 70 "-0... "-0... 60 ~ ..J o Ul w N 20 '" c) a 70 10 15 o o "- _1 EE o 01 OJ 80 EE o o " 90 80 Ul W 0:: o o (j) 100 90 b) 5 o lfJ RADIAL DISTANCE(mm) 15 50 ~ ..J o 40 Ul W 0:: 30 0:: 70 60 50 40 30 20 20 10 10 o '" o m o " o lfJ o (j) o " o OJ o 01 000 o RADIAL DISTANCE(mm) '" o m o " o lfJ o '" o m o (j) o " o OJ o 01 RADIAL DISTANCE(mm) Fig. 3. Data Evaluation Method: (a) Resolving Power for various radial distances. (b) Deriving 'resolution curves' by averageing over radial intervals of ~ r ~ 25 rrm. (c) Standard deviation of resolving power values. Left: Lines in flight direction (R) Right: Lines perpendicular to flight direction (T). 1... 1 o lfJ lSS 9:J 8::; E E ~ "-CL Z 0 68 5S I- :::J -l 0 UJ .:;.0 3(-: W 0:: RADIAL DISTANCECmm) RADIAL DISTANCECmm) ;00 90 80 E E ~C "-CL 60 Z 0 I- 50 :::J 40 UJ 30 -l 0 W 0:: 2D is C 1 , l 3 1 , R PAN-X Y: N: "-CL t Z 0 t. I- :::J i- UJ r ~ ~ L'i",,', "I""I,,!!I"!!h~-'--liL~~~-LJ.1-'-.LuL.-,-.LlJ 0 -, 0 (,J 0 '" 0 '" II (Q , U 0 III 0 OJ (J) 0 U 5_~_~ 0 .,:- LJ "J LJ '" RADIAL DI ST ANCE Cmm) C] c) c·; "" ______________ y, N, C" -, D lJ (n D III (J III 0 G1 0 (J D 0 0 OJ 01 0 0 0 (J " 1Il 100 WITH FMC NO FMC 90 80 70 E ~~~~ "-CL 60 W 0:: lJ RADIAL DISTANCECmm) 80 UJ -tD 3:': W 0:: 90 I:::J -l 0 51: -l 0 PAN-X Z 0 WITH FMC NO FMC y, N, 9L: Be; 100 E T EE 0 E 3 PAN-X WITH F~IC NO FMC 50 40 E 50 Z 0 I:::J -l 0 ~--¥ 30 70 "-CL UJ W 0:: 50 40 30 20 20 10 10 S 0 €\I 0 m 0 '" (J 1Il 0 to 0 r-- (J III 0 Ol 0 0 RADIAL DISTANCE Cmm) 0 0 €\I 0 m 0 '" 0 1Il S (J €\I 0 m 0 " 0 1Il 0 to 0 r-- 0 <D 0 Ol 0 0 RADIAL DISTANCECmm) 0 €\I m 0 " Fig. 4: Resolution Curves of RV1K A 15/23 with Panatomic-X film for contrast ratios 1 20, 1 3, 5 1 and for FMC on and off. Left: Lines in flight direction (R). Right: Lines perpendicular to flight direction (T) • 1... 180 0 1Il 100 100 90 90 80 E E "-0.. Z 0 -l 0 E 60 "-0... 50 Z 40 ~ E W 0:: 40 30 g 0 N 0 en ... 0 0 0 CD 0 0 <D 0 0 " rn ~ 0 g RADIAL DISTANCE (mm) If} IDO 0 0 en g ~ '" N: 50 0 ~ (J) 30 E Z "--~ 0 ~ ::J -l 0 (J) W 0:: 0 If} WITH NO ~ 40 30 20 10 10 g ... ~ 0 N 0 0 0 fil CD0 " 0:> rn 8 RADIAL DISTANCE(mm) 0 ~ 0 100 N, 90 0 0 en y, PLUS-X g 0 If} '" 0 N 0 en ':i 0 If} 0 CD ~ 0 <D 0 rn 0 0 0 ~ ~ ~ 0 ~ RADIAL DISTANCE (mm) 100 WITH NO y, PLUS-X N: 90 WITH NO 80 80 E N: .,. 0 60 50 W 0:: "-0.. Y: ~ 70 20 E 0 N 80 E "-0.. 40 -l 0 g 0 0 0 fil CD0 " <D al 0 RADIAL DISTANCE(mm) PLUS-X "0... ::J 0 90 80 60 ... ~ 0 N 100 WITH NO Y: PLUS-X 90 Z ~----v 10 0 ~ ~~~ 20 10 70 60 50 (J) W 0:: 20 ~ WITH NO 70 ::J -l 0 30 (J) N: 80 70 0 ~ ::J Y: PLUS-X E 70 E "-0.. 60 Z 70 60 50 50 0 40 ::J 40 (J) 30 ~ -l 0 ~~ 30 20 W 0:: ~ "-~ , 20 10 10 0 g 0 N 0 en .,. 0 0 0 0 0 fil 0 " 0:> rn 0 RADIAL DISTANCE (mm) If} 0 0 N 0 en .,. 0 ~ g 0 N 0 en .,. 0 0 If} 0 CD 0 " 0 0:> 0 rn 0 0 0 ~ ~ RADIAL DISTANCE (mm) Fig. 6: Resolution Curves of RMK A 15/23 with Plus-X film for FMC on and off. Left: Lines in flight direction (R) • Right:: Lines perpendicular to flight direction (T) • 1-181 .,.0 0 If} 100 90 80 E E 70 " 60 0... Z 0 50 f::J -.J 0 40 30 (j) W 0:: 20 10 0 20 1 [ 8. l NO 60 z 50 0... 0 t f::J -.J 0 (j) W 0:: ~ ~~ 40 ----j §- 10 g",1""1""1""1""1""1,,,,1,,,,1,,,,1,,,,1,,,,1""I,,! ,1""1,,,,1 a C\J a 01 \i' a 1f1 a 0 0 r· (0 00 0 01 a a a a C\J a 01 a a <t a S lfl a a a a a a 1f1 " til 01 0 RADIAL DI ST ANCE Cmm) a 01 C\J (j) E 70 " 60 E 5 Z 0 f::J -.J 0 40 (j) 30 40 ~-~ 30 N--~~ 20 20 10 10 S a C\J a 01 a <t a 1f1 a a a 0 00 " (0 OJ a a a 0 C\J 0 01 a <t a S If) RADIAL DI STANCE (mm) 5 100 , R 1 90 WITH Ft~C NO FMC (j) 0 <t If) FMC FMC WITH NO 60 " 60 50 Z 0 E 0... W 0:: 20 10 0 <t a til 001 a0 RADIAL DISTANCE (mm) 0 In (0 0 0 " 0 C\J 0 01 T :;3. y, WITH No NO ... 0 a 1f1 FMC 1 FMC, 50 H f::J -.J 0 40 30 0 01 N 80 70 " f.::J -.J 0 0 01 --y.-----~ -----r; 90 E 70 Z 0 Yo No D-X 80 E 0 '" ------.. 100 Yo No D-X 0... J. D-X 0 C\J 50 W 0:: W 0:: E 0 a 0... 50 f::J -.J 0 a (0 <t 80 80 Z 0 --~-y 20 90 60 ----~ 30 90 E NO 70 E " 100 0... FMC ' FMC WITH 80 100 " Yo No 90 RADIAL DISTANCECmm) 70 T 20 D-X E S E , 1 100 Yo No D-X l~~"~~~~,~~""~"~",,,~, S 0 C\J 0 01 0 " 0 If) 0 (0 a " 0 00 a 01 0 0 RADIAL DI STANCE (mm) 0 (j) ~-==--='~~~----'l\f---__~ 40 30 "( W 0:: 20 10 ""1,,,,,,,,,1,,,, 1 '" m " 0 0 0 0 S If) a C\J 0 m 0 " a If) a (0 0 " 0 00 a 01 a 0 0 0 OJ 0 en a <t RADIAL DISTANCE (mm) Fig. 7: Resolution Curves of fu~K A 15/23 with Double-X film for contrast ratios 1 20, 1 J , 5 1 and for FMC on and off. Left: Lines ln flight direction (R). Right: Lines perpendicular to flight direction (T). "') 1... 182 0 If) 90 100 1. :20 f· 70 is 50 ~ f.- 60 :.:J 40 ~ 30 20 90 t I 60 is 50 f.- e= -- . - -B- -::--::;::-:::::-::--:::::'~--o..=~~~ - :.:J 40 6 30 (Jj W t:r: - 20 s I ~~ ~~ 13-_~ --~-~ 0 OJ 0 01 0 ,t 0 lf1 0 (!J 0 "- 0 CD 0 OJ 0 0 0 0 N 0 01 ... 0 L : 3 CIR-2443 100 0 N S 0 0 " 01 81:J ..J 0 (Jj W 30 [J:: 20 10 0 _"I'="~I~"'~'d~ ~I~" 'd'U:I" I" I:" "': i 0 N 0 01 ... 0 51 0 (f) 0 "- 0 CD 0 OJ 0 0 RADIf.L DISTANCECmm) "0... 0 0 N 0 m 0 " 8 60 Z 0 50 I:.:J ..J 0 (Jj 0 lf1 40 30 10 0 lf1 S 100 100 90 90 80 80 0 N 0 01 0 " 0 lf1 0 (f) g 0 "- 0 OJ § 0 0 N E 70 E '... 70 50 .. 0 0 01 RADIAL DISTANCECmm) .GIR C-- 0--0 CIR-SO-131 R T Q. 60 60 Z 0 40 I:J ..J 0 (Jj 0 " 20 50 0 0 m RADIf.L DISTANCECmm) W Z 0 ~ 0 N [J:: 8 I- I", ,I",,! ""; I' 0 0 0 0 OJ CD 70 "-0... I S EE 0 "- 80 EE 70 40 0 (!J 90 80 50 0 0 lf1 100 R T 0--0 90 Z I 0 " 1"" I"" I"" I"" 1'1" I", ,I"" I"" I"" I"" I" 0 lf1 RADIAL DISTANCECmm) 60 I 10 0 ' " I"" I"" I"" I"" I"" I"" I""!",, I"" I"" I"" I, '" I"" I"" "0... _., 80 10 EE .. R T 0--0 CIR-SO-131 80 ~ LL.2.Q 100 R T 0--0 CIR-2443 (Jj 30 W W 40 30 [J:: [J:: 20 20 10 10 o N Rf.DIAL DISTANCECmm) o " o lf1 o (f) o " o CD o Ol o o o N o 01 ...o RADIAL DISTf.NCECmm) Fig. 8: Resolution Curves of ru~K A 15/23 with CIR-2443 film (left) and SO~131 film (right) for the contrast ratios 1 20, 1 3 and green/red (G/R). 1-183 0 lf1 1: 20. C-5o.-242 100 90 80 80 EE EE 70 "-0.. "-0.. 60 70 60 Z 0 50 is 50 I::J 40 ~ 40 0 W 0::: - ..J ...J (J) 3.M M= CR+T) /2 *--* T 90 1 : IDe 0--0 R o 30 (f) 30 W 0::: 20 20 10 10 - ,,/,,,,1,,,,1.,,,1,,,,1,,,,1,,,.1,,,,1,,,,1,,,,1 o 000 ... III to (!) o 0 Ol (!) RADIAL DI5TANCECmm) RADIAL DI5TANCECmm) 1 : 3 C-5o.-:242 :00 0--0 *--* 90 E E 70 "0.. Z 0 I::J ..J 0 (f) W 0::: 90 80 E E "0.. o ~ 60 -------~-----a '---.. 50 40 70 60 z 50 I::J 40 (J) 30 0 30 ..J 0 20 W 0::: 20 10 ~ ~ ~ ~ ~ ~ ~ @ § g ~ ~ ~ G/R C-5o.-242 100 90 E 60 ---.,.C-So.-242 -~ --~ -------~-5o.-131 ~443 RADIAL DISTANCECmm) 0--0 *--* Fig. 10: Average Resolution (00) of RMK A 15/23 with the films Panatomic-X, Plus-X, Double-X, CIR-2443, 80-131 and 80-242 for a contrast of 1 3. R T 80 "-0.. ------------ ~ RADIAL DI5TANCECmm) 70 -- ---------- 10 9 E 3 M M= CR+T) /2 --~~ 80 1 : 100 R T ~ ~ ~---~---------- 50 ~ 40 .. ..,. ~'---tI 30 20 " t"""",,,,,,,,,,,,,,,,,,,,,,,,,,,,,,,,,,,,,,,,,,,,,,,""""""""" a 0 N '" 000 m 01 ~ o N RADIAL DISTANCECmm) Fig. 9: Resolution Curves of RMK A 15/23 with 80-242 film for the contrast ratios 1 20, 1 3 and green/ red (G /R) . 1... 184