surveying iii (topographic and geodetic surveys) - Modern Prepper

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Figure 1-17. Astro-Geodetic Deflection of the Vertical(e) It is possible to produce a profile of the geoid with respect to the chosen referenceellipsoid if a certain number of Laplace stations are given in a geodetic net. This profile can then answerthe question of whether the adopted reference ellipsoid properly represents the curvature of the earthover the area being surveyed. The profile in Figure 1-18 indicates that between 50° north and 25° north,along the 98th meridian, there is nothing more than random deviations from the referenced Clarkeellipsoid. However, at 40° south the difference between the geoid and the ellipsoid approaches 200meters.EN0593 1-28
Figure 1-18. Geoid Profile of the 98th Meridian(f) Astro-geodetic datum orientation is obtained from the deflections of the vertical at anumber of selected Laplace stations (Figure 1-19). In this orientation method, the geoid and the ellipsoidare oriented so that the sum of the squares of the deflections of the vertical at the Laplace stations ismade as small as possible. One of the Laplace stations in the adjustment is arbitrarily selected as theorigin. Consequently, instead of having a zero deflection as with the single-point orientation, there is adeflection of the vertical at the origin point. Through a similar process, the geoid separation at thestarting point can be found. This procedure reorients the ellipsoid so that it provides the best average fitat all the Laplace stations. The use of geodetic data produced by this method is still limited to relativelysmall areas since the deflections of the vertical still remain relative. They are not comparable withsimilar deflections derived from another adjustment. As in the single astronomic method, the datum isnot earth-centered and the rotational axis of the ellipsoid does not coincide with the axis of the earth.1-29 EN0593
Page 1 and 2: SUBCOURSEEN0593EDITIONAUNITED STATE
Page 3 and 4: TERMINAL LEARNING OBJECTIVE:ACTION:
Page 6 and 7: Part G: Adjusting Precise-Positioni
Page 8 and 9: PART A - FIGURES OF THE EARTH1-1. T
Page 10 and 11: Figure 1-2. Flattening Fractiona. T
Page 12 and 13: 1-3. Geoid. In geodesy, precise com
Page 15 and 16: point in the survey to provide the
Page 18 and 19: one side of a triangle and all of t
Page 20 and 21: Figure 1-10. Simple Triangulation N
Page 22 and 23: observation, contains a light sourc
Page 24 and 25: of a horizontal rod with a small sp
Page 26 and 27: The Airy theory, announced by G. B.
Page 28 and 29: Figure 1-15. Products of the Gravim
Page 30 and 31: a. If the shape of the earth was ex
Page 32 and 33: Figure 1-16. Single Astronomic Stat
Page 36 and 37: Figure 1-19. Astro-Geodetic Datum O
Page 38 and 39: (c) The significance of a gravity-o
Page 40 and 41: absolute deflections of the vertica
Page 42 and 43: Figure 1-23. Preferred Datumsa. The
Page 44 and 45: 1-17. The World Geodetic System. Be
Page 46 and 47: Figure 1-25. Using the Same Referen
Page 48 and 49: LESSON 1PRACTICE EXERCISEThe follow
Page 50 and 51: 12. Which of the following is assum
Page 52 and 53: LESSON 1PRACTICE EXERCISEANSWER KEY
Page 54 and 55: THIS PAGE IS INTENTIONALLY LEFT BLA
Page 56 and 57: for all military and civilian activ
Page 58 and 59: i. Additional support for other top
Page 60 and 61: 2-7. Status. At present, topographi
Page 62 and 63: in both. (North American Datum of 1
Page 64 and 65: water can impede leveling operation
Page 66 and 67: A field recording booklet. A single
Page 68 and 69: PART I - OFFICE WORK2-24. General.
Page 70 and 71: PART J - SURVEY COMMUNICATION2-28.
Page 72 and 73: length or side is known, and all th
Page 74 and 75: second-order, Class I net. The leng
Page 76 and 77: The number of observations required
Page 78 and 79: to perform the reconnaissance. Fail
Page 80 and 81: and cultivated, or fields may have
Page 82 and 83: e an alphanumeric symbol that is st
Page 84 and 85:
2-53. Intervisibility of Stations.
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station is (K/2) 2 x 0.0676, or one
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Figure 2-8. Similar Triangles Solut
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2-54. Height of Obstructions. It is
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authorized to change the name, it s
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Figure 2-12. Cells Connected in Par
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added as the cells weaken. Three un
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Figure 2-16. Construction Details f
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2-60. Wooden Towers. When it become
Page 102 and 103:
LESSON 2PRACTICE EXERCISEThe follow
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11. The face of the 5-inch signal l
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LESSON 2PRACTICE EXERCISEANSWER KEY
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average line in a triangulation sys
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3-4. Slope Measurements. The slope
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strip as close as possible to its f
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. Sight along the tops of both of t
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Column 1. Record the station number
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stake to steady it. With the back o
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Figure 3-3. DA Form 4446 (Sample of
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micrometer in this optical system i
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laterally across the front of the e
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Figure 3-7. Horizontal Circle and M
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out of adjustment. If the index mar
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(1) In order to avoid instrumental
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location of the vertical circle on
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Figure 3-13. Open Traversec. Closed
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designate the exact point of refere
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example, a line with an azimuth of
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When adjusting a traverse that star
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11. The unit of graduation on a hor
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THIS PAGE IS INTENTIONALLY LEFT BLA
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differential leveling. The theodoli
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additional runs are made due to exc
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Figure 4-2. Wild N-3 Precision Leve
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(8) Loosen the azimuth clamp (13),
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4.7. Miscellaneous Equipment. In ad
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(2) To check for gross errors in th
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(a) (1) Begin by completing the inf
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Set up and level the instrument. Re
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Figure 4-8. Sun and Wind Code(5) Th
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(10) Enter the interval between the
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Figure 4-9. Closed-Circuit River Cr
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Figure 4-11. Sample DA Form 5820 (R
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is 0. When the telescope is pointed
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stations. However, since all statio
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a. Complete the heading, as shown.b
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a. (1) Enter the date, as in the sa
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11. The maximum length of site to o
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PART A - GLOBAL POSITIONING SYSTEM
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5-7. Pseudorange. A pseudorange is
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5-15. Number of Pseudorange Observa
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i. Probable Error Measures. The acc
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Table 5-1. Representative GPS Error
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Table 5-2. Carrier Phase Trackinga.
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exercise extreme caution in applyin
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not be designed or performed to ach
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Table 5-3. GPS-S Design, Geometry,
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f. Multiple/Repeat Baseline Connect
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possible ionospheric and tropospher
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Figures 5-4. PDOP Versus Time PlotP
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e. Field Processing and Verificatio
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All carrier phase relative-surveyin
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time spent and the cost of conducti
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movement between occupation sites,
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5-37. General. GPS baseline solutio
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(1) Receiver Time. This technique u
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NOTE: Repeated baselines should be
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5-43. Loop Closure Checks. Postproc
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necessary to determine approximate
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This will ensure that future work w
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may (and usually does) far exceed t
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important in evaluating the overall
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i. Relative GPS baseline standard e
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12. When the networking method is s
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THIS PAGE IS INTENTIONALLY LEFT BLA
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FAR-77 obstructions. Aircraft-movem
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Figure 6-1. Imaginary SurfacesEN059
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Figure 6-3. Approach Surfacesa. Fed
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. Federal Aviation Regulation-77, S
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Table 6-4. Airport Obstruction Accu
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A horizontal scale of 1:12,000 and
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Figure 6-4. Sample DA Form 5821 (Ai
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Figure 6-5. Sample DA Form 5822 (PA
Page 262 and 263:
Page 264:
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