TABLES 7 AND 8, AND SECTIONS 27, 28, AND 29 OF THE BOOK AEROLOGY, WHICH DEAL WITH PILOT BALLOON OBSERVATIONS AEROLOGIYA

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Document Number (FOIA) /ESDN (CREST): 
CIA-RDP82-00039R000200010042-3
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RIPPUB
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R
Document Page Count: 
31
Document Creation Date: 
December 22, 2016
Document Release Date: 
April 3, 2012
Sequence Number: 
42
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Publication Date: 
April 29, 1952
Content Type: 
REPORT
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PDF icon CIA-RDP82-00039R000200010042-3.pdf10.81 MB
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Declassified in Part - Sanitized Copy Approved for Release 2012/04/03 : CIA-RDP82-00039R000200010042-3 A. B. Kalinovskiy and N Pinus IMPORTJNT NOTE : The content of this report is UNCLASSIFIED and may disseminated U':1~1CLASSIFIED at the discretion o appropriate recipient offices. If such disseminationis must be detached made, however, the RESTRICTED cover-sheet mus and neither the Central Intelligence Agency nor the US GoverTrrr1ent be. cited as the source of this work. Declassified in Part - Sanitized Copy Approved for Release 2012/04/03 : CIA-RDP82-00039R000200010042-3 Declassified in Part - Sanitized Copy Approved for Release 2012/04/03 : CIA-RDP82-00039R000200010042-3 TABLE ? pilot ~ai1oon No7 Date 6 March hour. 6 minutes 1G Casing No 20 Free lifting r Length of circtiunference 2force ,ce 23~ ~ Vertical velocity 223 rn/min Corrected for density 2111 m/rnin Correction Multip11er 096 nt No Wind at standard altitudes base No poa. Over land surface pressure 7.6.2 mm, 99409 mb Temperature ~ by dry " 3o0 ia, velocity direction by wet - 3?~ Humidity. relative 56% absolute L.2 mm theodolite system Above sea level Vera.f.icatlon ?f the Sh2 km velocity direction before ascent after ascent angle direct inverted direct inver?sight sight sight ted sight hox'izontal vertical before as after as- cent cent Cloudiness amount of gen/lower and form Wind: (by vane) ; di- rectionand velocity Reason for stopping observation entered pc Declassified in Part - Sanitized Copy Approved for Release 2012/04/03 : CIA-RDP82-00039R000200010042-3 STAT Declassified in Part - Sanitized Copy Approved for Release 2012/04/03 : CIA-RDP82-00039R000200010042-3 . . tered over land surd. ac 5ignature of observers Declassified in Part - Sanitized Copy Approved for Release 2012/04/03 : CIA-RDP82-00039R000200010042-3 The Balloon went in direction bal:l.oon (an momen~' tm and height of cloudS, 1n e which ~'o .. ................ .~o..~. P.~ are--~ 1 ev ................ Declassified in Part - Sanitized Copy Approved for Release 2012/04/03 : CIA-RDP82-00039R000200010042-3 rjiA~aj! 6 7 covered by Frst 8 Alt9.tude Altitude Verti- ave, layer of balloon cal over above Wind over land velow V/ land sea dir. ec- vel.o- surface city sur..level Lion city Declassified in Part - Sanitized Copy Approved for Release 2012/04/03 : CIA-RDP82-00039R000200010042-3 Minutes readings Declassified in Part - Sanitized Copy Approved for Release 2012/04/03 : CIA-RDP82-00039R000200010042-3 27 Errors in the Method of-Pilot~l.oonMOb ervatiOflS :from One point The method of pilot balloon observations from one point, as also other methods, makes it possi.ble to determine the speed and dire.;tion of the wind with a certain degree of accuracy de- pending on the size of errors in the obtained results. Knowing the size of these errors permits us to judge the area of appli- cation of this method and to avoid large errors in the utilizaw tion of the results obtained. Inasmuch as the wind velocity and direction are determined by the size and direction of the segments between the projections of the pilot? balloon, then, consequently, the errors in the deter- urination of the positions of the projections will result in errors the determination of the wind velocity and direction. The in p.rojections in turn depends on the values of the position of the coordinates of the pilot balloon, ire., azimuths, vertical angles, altitudes? In this manner, the errors in the determination of and the wind velocity and direction depend on the errors of the basic values forming the foundation of the method, namely, the azimuth, the vertical angle and the altitude? In studying the question of errors and the determination o the wind velocity and direction those errors in the determination of ~ angular coordinates which are accidental are taken into account, assuming that the systematic errors are corresponding corrections, considered by means of The error in the determination of he altitude of the pilot balloon error is? considered to be dependent on the -n the determination of the vertical velocity, assuming that Declassified in Part - Sanitized Copy Approved for Release 2012/04/03 : CIA-RDP82-00039R000200010042-3 Declassified in Part - Sanitized Copy Approved for Release 2012/04/03 : CIA-RDP82-00039R000200010042-3 the interval of taare from the moment of release of he pilot balloon to the reading is correct. ..._w... ~La?...s...ni.os _.: at _th~ effeCt of errors in the determination of coordinates of the pilot balloon upon the relative error in the determination of the wind. Let us assume that at some moment of time t1 the horizontal projection of the pilot balloon is at point Cl, and at the next moment of time t2 ~- at point 02 (Figure ;3(). The segment 0102: 1 represents the displacement of the pilot balloon for the interval of time t2 - tl. The velocity of the wind for layer H2 w Hl is therefore determined by [ diagram page 80] Figure 7. The effect of error in the determination of azimuths. The relation for the distance between projection 1 to the interval of time t2 - tl is [formula page 3l]. The relative error in the determination of the wind velocity= a.ysuminp that the error in the determination of t2 - tl is equal to zero mate expressed in the form; [formula page 81] . (5C)) In t, LS manner the determination of the relative error in the magnitude of the wind velocity is reduced to the determination of ` Declassified in Part - Sanitized Copy Approved for Release 2012/04/03 : CIA-RDP82-00039R000200010042-3 Declassified in Part - Sanitized Copy Approved for Release 2012/04/03 : CIA-RDP82-00039R000200010042-3 Declassified in Part - Sanitized Copy Approved for Release 2012/04/03 : CIA-RDP82-00039R000200010042-3 the relative errors in the horizontal displacements oi' the balloon. Let us look at the errors in the determination of the wind 1 ination velocity a,nd_ ci rectian which depend on the errors in the deter.~m .... of azimuths. Let us assume first of all that the errors in the determinations of azinuths at moments tl and t2 are equal in size and sign and equal to A ;4;. Then the projections Cl and 02 Will appear at points Ci and C' and the triangle 00102 whose angle () is equal to the 2 difference of the azimuths will take up the position OC~C, and the segment C1C?. will turn through the angle \ OK a In this manner the constant error (Y.. in the determination of the wind velocity will not show any effect, and the error in the deternii.nati.on of the direction will. be equal to the constant error L +. r Such an error may appear in the case of an incorrect orientation of the theodolite If the theodolite is oriented. with an error of about 1 to 2 degrees then the determination of the direction will not be affected. If the errors in the determination of azimuths are different, this case may be reduced to that where one of the azimuths is determined correctly and the other with an error, equal to the difference of errors in the determination of both azimuths. In Figure 8 the segment C C2 = 1 represents the actual displacement of the 3 ~ 1 balloon and segment C C', the displacement due to error Li CX in the 12 determination of the value of angle from point 02 to segment C1C 'i 2. Dropping a perpendicular we may state that the error in the determination of value 1 will be equal to the magnitude of segment rC Declassified in Part - Sanitized Copy Approved for Release 2012/04/03 : CIA-RDP82-00039R000200010042-3 From the right angle triangle rC2C it fo11ows that Cformula he 8l], where T2 st,a from the point of observation 0 to the ~.hs the da.,, ,r .ce f ro projection 02 and is the angle C CO. E3esides than at may be ~ 1 2 approximately asi ned that C2C~ G ? s 2 1 diagr a page 81] Lion of errors in the wind velocity and direction Figure 38. Computa a to errors in the determination off' t} azimuths. duc. Replacing ~ c: ~ 2 by L q;' we will obtain for the absolute ~n the determination of the wand the expressions and r. e1at~-ve erro . .~ ? ~- `formula page 82], ) ) ) [formula page 82], ) error in the measurement of the dLfferefCes of where the the azimuths, The error in direction will be obtained, after determining angle segments C. C2and ClC' By utilizing the triangle ,~+ ~~ , by l 2 C1C2C we can state [formula page 82]d In view of the small value of )`( , let us substitute approximately and, besides, L2 L.~. fo1-sine '1. w [formula page 82] for C2C2 Then, (52) Declassified in Part - Sanitized Copy Approved for Release 2012/04/03 : CIA-RDP82-00039R000200010042-3 Declassified in Part - Sanitized Copy Approved for Release 2012/04/03 : CIA-RDP82-00039R000200010042-3 The expressions (:L) and (a~2) show that gnawmuch as thr. relative error in the determination of the wind velocity is t4' . ,y` s c.? = ::. then the eerror in the wind direction L\ l( increases with the increase of L\ and the relation -r. and, an addition 1 depends on the size of the angle Let us study the errors in the detenninataon of the wand velocity and direction which depend on he errors in the determination of the vertical angles o In Figure 39, the triangles POC and P10C1 represent pilot balloon triangles in which OC is the distance to the projection of the balloon in a correct determination of the vertical angle, and 0C1_, the distance obtained with an error caused by an error in the determination of the vertical angle '\ From studying the triangle OP1P it follows that [formula page 821. [diagram page 82] Figure 39? The effect of errors in the determination of the vertical angleq L?L cos L, The value OP may be represented as _-2, or in the form of c~ cos 6 Disregard:Lng in the numerator of this expression the value and also the value rr'~ k in sin relation may be restated in the form [formula page 821, from where ), the preceding Declassified in Part - Sanitized Copy Aproved for Release 2012/04/03 : CIA-RDP82-00039R000200010042-3 Declassified in Part - Sanitized Copy Approved for Release 2012/04/03 : CIA-RDP82-00039R000200010042-3 formula page 8. (3) /. In formula (~.~), in view of the small value o:C angle we shall substitute the angle itself for. its sine. It determines o,C the errors in the measurement of the vertical angle the effect in the determination Of the distance to the projection an the error of the pilot balloon. It is not difficult to see that in the given L and L 8 , its maximum value for , L is reached at small magni- tudes of S or near 90 degrees. Inversely, the minimum value for L takes place when angle is close to L degrees. Let us assume that errors in the determination of the vertical angles effect the determination of distances to projections C1 and C2 the length of segments 0C and. 002 (Figure Lo), in such a manner that [formula page 83] or, as f ollo? s from formula (53) [formula page 83] Evidently, in this case the triangles 00102 and OCjC are (SL) similar. The segment C[C~ represents the distance between the pro- jections, obtained with error rC. The magnitude of this error may be determined by the relation [formula page 83]. [ diagram page 83] Figure L.O. The effect of error in the determination of vertical angles. Declassified in Part - Sanitized Copy Approved for Release 2012/04/03 : CIA-RDP82-00039R000200010042-3 Declassified in Part - Sanitized Copy Approved for Release 2012/04/03 : CIA-RDP82-00039R000200010042-3 Replacing 2 from the relation (L), we obtain , ~ n`' 2 [formula page 83a? a suf'fiCient da stance of the baa.loon, the value rC will \ L2 /r..,, will be L2_ be consequential, because the relation = small. C As a resrult of the fact that under a normal value 0f O , for a great distance of the balloon, the values 1 and 2 will be close to each other., then in order to satisfy the relation (,~1a), it is necessary that and Z