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12.010 HW 3 Solution 1 10/30/2000. 12.215 Homework #3 ... - MIT

12.010 HW 3 Solution 1 10/30/2000. 12.215 Homework #3 ... - MIT

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<strong>12.0<strong>10</strong></strong> <strong>HW</strong> 3 <strong>Solution</strong> 1 <strong>10</strong>/<strong>30</strong>/<strong>2000.</strong><br />

<strong>12.215</strong> <strong>Homework</strong> <strong>#3</strong> <strong>Solution</strong> Due Monday <strong>10</strong>/<strong>30</strong>/2000<br />

Latitude and Longitude determination.<br />

(a) Find the time and the value of the maximum angle between the sun and its reflection<br />

using the data given below (Note: Acroread has an option that allows text to be<br />

copied from a PDF file, therefore it should not be necessary to re-type any of the<br />

values). (<strong>10</strong> points)<br />

Sextant <strong>10</strong>/00<br />

75<br />

74<br />

2*Sun Elev (deg)<br />

73<br />

2*Sun Elev (deg)<br />

73<br />

72<br />

72<br />

72<br />

71<br />

Y = M0 + M1*x + ... M8*x 8 + M9*x 9<br />

M0<br />

-858.71<br />

M1<br />

113.17<br />

M2<br />

-3.4318<br />

R<br />

0.99882<br />

70<br />

15.4 15.6 15.8 16.0 16.2 16.4 16.6 16.8<br />

GMT Hrs<br />

The plot of the data collected in class in shown in the above figure. The quadratic fit<br />

to the data is shown in the box.<br />

2<br />

2ε( t) = − 857. 71 + 113. 17t − 3.<br />

4318t<br />

d( 2ε( t))<br />

d( 2ε( t))<br />

= 113. 17 − 2 × 3.<br />

4318t<br />

⇒ = 0 when t = 16.4884 hrs<br />

dt<br />

dt<br />

By setting the derivative to zero, the find that:


<strong>12.0<strong>10</strong></strong> <strong>HW</strong> 3 <strong>Solution</strong> 2 <strong>10</strong>/<strong>30</strong>/<strong>2000.</strong><br />

(a) Sun reached maximum elevation at 16.4884 hrs UT = 16 hrs 29 min 18 sec<br />

(b) Find the mean index errors for the near and distance objects (5 points)<br />

Mean index error for nearby objects is 11.0’<br />

Mean index error of distant objects is 14.9’<br />

(c) At the time of the maximum angle between the sun and its reflection, find the right<br />

ascension (RA) and declination of the Sun, and the Greenwich Mean Sidereal Time<br />

(GMST). You can use the nautical almanac in Lindgreen Library or the on-line<br />

almanac referenced on the course web page. (<strong>10</strong> points)<br />

From the web site http://aa.usno.navy.mil/AA/data/docs/WebMICA_2.html that directly<br />

allows calculations of the positions of astronomical positions we obtain for the<br />

topocentric position of the Sun (these positions refer to a coordinate system whose origin<br />

is at the surface of the Earth. An approximate position must be given for these positions).<br />

2000 Oct 20 16:29:18.0 (UT1)<br />

Object R.A. Dec. Dist. Z.D. Az. Elong. Diam. Mag<br />

h m o ' A.U. o o o ' "<br />

Sun 13 42.4 -<strong>10</strong> 37 0.995 51 181 ---- 32 08.0 ----<br />

The other type of position is geocentric, apparent (meaning the value that would be seen)<br />

coordinates and these are given below for the Sun. These values should differ at most by<br />

the radius of the Earth divided by the distance to the sun (approximately 8.8”).<br />

Date Time Right Declination Distance Equation<br />

(UT1) Ascension of Time<br />

h m s h m s o ' " AU m s<br />

2000 Oct 20 16:29:18.0 13 42 25.924 - <strong>10</strong> 36 46.37 0.9955135<strong>10</strong> +15 18.5<br />

Greenwich Sidereal time has its own look up table and the value is.<br />

Date Time Sidereal Time<br />

h m s h m s<br />

2000 Oct 20 16:29:18.0 18 27 03.5<strong>10</strong>3<br />

RA of Sun 13h 42m 25.92s 13.7072 hrs<br />

Declination of Sun -<strong>10</strong> o 36’ 46.37” -<strong>10</strong>.6129 deg<br />

GST 18h 27m 03.51s 18.45<strong>10</strong> hrs<br />

(d) Using the mean index error for distance objects, compute the elevation angle to the<br />

Sun at its maximum (5 points)


<strong>12.0<strong>10</strong></strong> <strong>HW</strong> 3 <strong>Solution</strong> 3 <strong>10</strong>/<strong>30</strong>/<strong>2000.</strong><br />

Based on the quadratric fit in part (a), the maximum value of 2*elevation to Sun is<br />

74.2879 degrees. Since when we knew the elevation angle was zero, the mean reading on<br />

the Sextant was 14.9’ (0.2483 degree), the index error should be subtracted from the<br />

above value and then divided by 2 to obtain the elevation angle.<br />

Maximum elevation of Sun = 37.0198 deg.<br />

(e) Compute the approximate atmospheric bending contribution to this measured<br />

elevation to the sun (<strong>10</strong> points)<br />

The refraction correction is 1’/(tan ε + 0.03).<br />

At 37.0198 deg., refraction correction is 1.3’ = 0.0213 deg which should be subtracted<br />

from the apparent elevation.<br />

(f) Given the declination of the Sun and the in vacuum estimate of the elevation angle to<br />

the Sun, compute the latitude of the Green building. (<strong>10</strong> points)<br />

The figure below shows the geometry of the latitude determination<br />

ε obs<br />

∆ε Refraction<br />

ε true<br />

To Sun<br />

φ<br />

δ (negative)<br />

To Sun<br />

φ = [90 - ( ε obs -∆ε ) + δ]<br />

The latitude, φ, is given by (90-ε c )-δ s = 42.3796 degrees = 42 o 22.8’ (Actual 42 o 21.6’)


<strong>12.0<strong>10</strong></strong> <strong>HW</strong> 3 <strong>Solution</strong> 4 <strong>10</strong>/<strong>30</strong>/<strong>2000.</strong><br />

(g) Given the RA of the sun and the GST when the sun was at its maximum elevation<br />

angle, compute the longitude of the Green building (<strong>10</strong> points)<br />

The longitude is RA s -GST = -4.7438 hrs = -71.157 deg = 71 o 9.4’ (Actual 71 o 4.8’)<br />

(h) What would be the effect on the results from parts (f) and (g) if the near object index<br />

error correction were used (<strong>10</strong> points)<br />

A change in the index error would effect the latitude (the effect is half the size since we<br />

observed a reflection). There would be no effect on longitude.

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