Continuation: TABLE N° 2 
TRIANGULATED STRIPS WITH THE INSTRUMENTAL METHOD 
  
  
  
  
  
  
  
  
  
  
  
  
  
  
  
  
  
  
  
  
  
  
  
  
  
  
  
  
  
  
  
  
  
  
  
  
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| | Bridging 
rcv lich | n OE inta iae N p. à eus hie © 
ae Flight | Ground contro lpoints T — re ee Adjustment of strips Reached precision 
rpose | | s . : : . L 
| | | Plotting instruments Bridging characteristics 
| | 2 
| | — | | 
| | I 
0 | Y : T | ToS 1 8 3 A TTT TR I T m 73: = + —————  a————— — TETE Tr mecs — —Óá —— en tr — AAT —————— — | — —— RE ee — = - 2 — I 
| Country | Organization map scale | | | | | | | | | | | 
| | | | m | Flight | | Overlap sa cod i. Tota s : Thermical \Onerators| Relative Use | Adjustme | T e | T 7 lean errors 
| | — | | Photo- | Camera | ind | moo 1 P | Auxiliary| Ground | dia Position of | | Plotting Preli- character Operators| nd | af data Time | N° of | Dave f| | Use of data Use Use of | Mean error: 
| | | ^ en : : 1. | altitude | 10t0 | anc ; | number : Hi : : ON £ | ridoi a | uU . | A. CISLOI | fr | pi — PANNE 
| | | total area | Cameras | gr aphic | calibra- | and | oro | strip equip- | character- for control points Type instru- minary istics Rd Bridging absolute | from | required | repe- B. refraction | Planimetry Altimetry irom | of 2d other | Tests 
| | | | | material | tion. | ras | Sc: | ments istics ! | in the strip | ments tosts of |W orking method orientation | auxiliary | for model | titions | C. film | | auxiliary | electronic | equip- x : 
| | | | | | | direction | | length | strips | | | | rooms | shifts of models |equipments| | shrinkage lequipments| computers | ment | | y z 
| | | | | | | | | | | | | | | | | 
| | LO Etre | — | —— | nm i | - ——— emia p = BEER ] us emen] umeris = | ee — ee 
| | | | | | | | — —— D aN — | —— I € — nere: = = | uu ud rs e S 
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12 | INDIA | Survey of India | | (film | | | |5-3-5 and a few A. 7 Stereosco-| Aircondi-|1 operat. | | Numerical relati-| {3 hours | A. Compensa-| Errors computed and adjusted | 
Department | | | | | | | | more for checks | | pic grid test tioned |2 shifts |ve orientation.| | | | ting plates|graphically 
| | | | | | for heights | Graphical for set- | | | |C. by f varia- | 
| | | | | ‚only Iting planimetry.| | | tion | | | 
| | | | | | | | | | | | 
|1 : 50.000 |R.C. 5 A | 20.000 ft.| 60 low and | | | | | | | | | | | | 
| | E-W 50 km ondulating | | | | | | | | | | | | | L 8 ft 
" | | | | | | | pS . 
| | (hills | | | | | | | | | | | x: 
| | | | | | | | | 
- a > | . | | | 
| : 50.000 Eagle IX | 16.000 ft. 60 plains in | | | | | | | | | | | | | | 
| | NW-SE 50 km Ithe foot | | | | | | | | | | | 
| | hills - jun- | | | | | | | | | | | | 
| | gle cove- | | | | | | | | | | | | | | | 
| | red | | | | | | | | | | | 
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67/1 mile RC. 5 À | 12.000 ft. 60 ondulating | | | | | | | | | 
| | | 150 km | | | | | | | | | | 
| | | | | | | | | | | | | 
137/1 mile RC. 5 À | | 12.000 ft.| 60 | | | | | | | | | | 
| | | 12 km | | | | | | | | | | | | 21742 
| | | | | i | | | | | | | — , 
| | . | | | | 
11:25.000 |R.C. 5 A| | 7.000 ft. 160 | hilly | | | | | | | 
1 : 15.000 | | E-W 12 km | | | | | | | | |+ 5 ft ) 
| | | | | | | | + + . 
| | | | | | | | | | | 
(1: 50.000 R.C. 5 À | | 124.000 ft. 160 | high hills | | | | | | 
| | IN-S | 77 km | with dense | | | | | | | | | | | | | + 8 ft 
| | | | jungle | | | | | | | | | ^. 
| | | | | | | 
| | | | | ed | | | | 
———— d re "| — uis cem | — € 7 —— FF | — =! —— mu — MÀ] lo = | áo = | | m Muir on 
^ ^ ^ m | | | | Mer, EY o" 5 poy { ts | . . | . . . | | | 
13 | IRAN N.C.C. 1 : 2.000 R.C. 5A |. | 1 : 10.000 | | |Every 2-7 models| A. 7 | Grid plate| Aircondi-|2 shifts |free Numerical  rela- |2 hours | Semigraphical, no | | | 
| : 2.500 | film | | LE 12.500 | | |ground control |test. tioned | tive orientation | |semianalytical | | | 
1 : 10.000 R.M.K. | | | |1 : 30.000 | | {points for planime- [Monocular | ladjustment| | | 
| | | | | | | Itry. Each model: test, stereo- | | | ‘method was| | | 
| | | | | | 3 elevation points |scopic test, | metodos | | 
1.225 km? | | | | | | | | grid plate | |using correc-| | | 
15 strips | | | | | | | | |A. 8 \triangula- Bonneval’s| Empirical relati- tion curves] | | 
| | | | | | | tion of 10- method ve orientation ((Zarzycki- | | 
| | | | | | 20 models | Brandt) | | | 
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| | | 
M aM —— | —— -|— ——— ——— | — | — a | nl | EK A — - —] (P —{ - — - —— sa -— - me | eee eee — — — — — — = — zl - MM — po | | Re 
i | | 
IL A.S.C. 16.000 km? Metrogon | | 2-4 models| | Multiplex Multiplex me- | | | | | | | | 
| | | | | I | | | | | 
115 strips | | | thod | | | | | | | | 
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— mins | ee a N | mE | € | UT | . ^ m] meer " | Free — |r| —— — | e om) en | = | [E = 
14 | ISRAEL | : 10.000 R.C. 5 A |film By l : 20.000 | | | 8 4 in the first model, natural de-|A. 5 Grid test, Aircondi- 2 shifts | Von-Gruber's| 4 models! | | Until recently strips were ad- | | | | |+ 2 m |+ 1,5 m 
f = 11,5 | | factory | l : 95.000 |20 km | | | 2 in the middle, 2 tails A. 7 monocular|tioned method - numeri- | per shift | |justed by the Brandenberger | | | 
| | | | | a | at the end. test, Stereo- rical orientation | | | |Zarzycki method, with the in- | | | | 
| | | | | | scopic test. | | | |terpolation done by calcula- | | 
| | | | | | | | Half yearly | | | |tions instead of graphically. 
| | | n | | | | checked. | | | |Only recently it is started | | | 
1 : 20.000 | |1 : 35.000 135 km | | | | | | | | | | | |adjustment by the method of | + 4m [+ 2,5 m 
1 : 50.000 | | | | | | | | least squares | | | 
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