Question: please help me with solving this problem and writing the code. ( using C++) The geographic location of a radar tracking site on the surface
please help me with solving this problem and writing the code. ( using C++)


The geographic location of a radar tracking site on the surface of the earth is known. Its geodetic latitude, longitude, and altitude above mean sea level are specified. Observations of a satellite are made by a radar at this site at a specified date and universal time. The radar determines .p.El. El. AzAz from its tracking and Doppler capability. Write a computer code to compute the geocentric-equatorial components of position and velocity of the radar site (rs and vs) and of the satellite (r and v). To accomplish this, it will also be necessary to write into your code a conversion from universal time to local sidereal time For 201716-1.738950248 rad-99.63451. Remember that the computer natively uses units of radians and you will have to make allowances for this. It may also be convenient to convert all length and time units into DU and TU units. Provide the requested solution (with proper units) for the following input data Data Set Lat (de Long (deg) 104.883 W 175.9W 78.5 W H (ft) 3 0.0N 80.040075 E 72.9 E 39.007 N 37.8 S 29.8 N 45.7 N 3610 1024:30 132 (13 Ma 897.5 0.57 76.7 0.48 201.7 0.75 7180 0317:02 0 1705:15 15 2210:57.5 0000:00 Day (2017) 234 (22 Aug) 57 (27 Feb) 357 (24 Dec 0 (1 Jan (km) | 404.68 (km/s) | 1.38 El (deg) El (deg/s) 0.07 300 6378.165 4.5 135 0.53 90 0.1 160 20.7 0.3 315 0.2 105.6 Ac (deg/s) 10.05 0.5 The geographic location of a radar tracking site on the surface of the earth is known. Its geodetic latitude, longitude, and altitude above mean sea level are specified. Observations of a satellite are made by a radar at this site at a specified date and universal time. The radar determines .p.El. El. AzAz from its tracking and Doppler capability. Write a computer code to compute the geocentric-equatorial components of position and velocity of the radar site (rs and vs) and of the satellite (r and v). To accomplish this, it will also be necessary to write into your code a conversion from universal time to local sidereal time For 201716-1.738950248 rad-99.63451. Remember that the computer natively uses units of radians and you will have to make allowances for this. It may also be convenient to convert all length and time units into DU and TU units. Provide the requested solution (with proper units) for the following input data Data Set Lat (de Long (deg) 104.883 W 175.9W 78.5 W H (ft) 3 0.0N 80.040075 E 72.9 E 39.007 N 37.8 S 29.8 N 45.7 N 3610 1024:30 132 (13 Ma 897.5 0.57 76.7 0.48 201.7 0.75 7180 0317:02 0 1705:15 15 2210:57.5 0000:00 Day (2017) 234 (22 Aug) 57 (27 Feb) 357 (24 Dec 0 (1 Jan (km) | 404.68 (km/s) | 1.38 El (deg) El (deg/s) 0.07 300 6378.165 4.5 135 0.53 90 0.1 160 20.7 0.3 315 0.2 105.6 Ac (deg/s) 10.05 0.5
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