(a) What are the underlying problems that led to the evolution of 2G radio systems? (b) Explain the steps to find the nearest co-channel neighbors of a particular cell? What is the cluster size

Materials Science And Engineering Properties
1st Edition
ISBN:9781111988609
Author:Charles Gilmore
Publisher:Charles Gilmore
Chapter15: Experimental Methods
Section: Chapter Questions
Problem 7ETSQ
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4.
(a) What are the underlying problems that led to the
evolution of 2G radio systems?
(b) Explain the steps to find the nearest co-channel
neighbors of a particular cell? What is the cluster size
when i=2 andj=1. Draw only all of its re-use cells.
Explain why the shape of a cell is HEXAGONAL?
(c) GhanaSat-1 carries low- and high-resolution
cameras that will be used to take pictures of Ghana,
monitor the country's coastline, and broadcast the
national anthem of Ghana. The satellite has the ability
to receive requested songs from the ground and play
them in space. Finally, the satellite will be used to
measure the effects of radiation in space on
commercial microprocessors. Calculate the apogee and
perigee heights for the following orbital parameters, e
= 0.004315, P= 90.57minutes,
The earth's geocentric gravitational constant is
µ = 3.986005 x 1014 m³ / s². Assume a mean earth radius R
is 6371 km.
Transcribed Image Text:4. (a) What are the underlying problems that led to the evolution of 2G radio systems? (b) Explain the steps to find the nearest co-channel neighbors of a particular cell? What is the cluster size when i=2 andj=1. Draw only all of its re-use cells. Explain why the shape of a cell is HEXAGONAL? (c) GhanaSat-1 carries low- and high-resolution cameras that will be used to take pictures of Ghana, monitor the country's coastline, and broadcast the national anthem of Ghana. The satellite has the ability to receive requested songs from the ground and play them in space. Finally, the satellite will be used to measure the effects of radiation in space on commercial microprocessors. Calculate the apogee and perigee heights for the following orbital parameters, e = 0.004315, P= 90.57minutes, The earth's geocentric gravitational constant is µ = 3.986005 x 1014 m³ / s². Assume a mean earth radius R is 6371 km.
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