written 6.8 years ago by | modified 2.8 years ago by |
Subject: Mobile Communication and Computing
Topic: Introduction to Mobile Computing
Difficulty: High
written 6.8 years ago by | modified 2.8 years ago by |
Subject: Mobile Communication and Computing
Topic: Introduction to Mobile Computing
Difficulty: High
written 6.7 years ago by |
Global Mobile Communication
Satellite Basics
Satellites in circular orbits
a. m: mass of the satellite
b. R: radius of the earth (R = 6370 km)
c. r: distance from the satellite to the center of the earth.
d. g: acceleration of gravity (g = 9.81 m/s²)
e. ω: angular velocity (ω = 2 π f, f: rotation frequency)
Stable orbit
From the preceding equation ,we notice that the mass of the satellite has no impact on its satiability as m appear on both side of the equation and get cancelled.
Fg = m g (R/r)²
Fc = m r ω²
Fg=fc m g (R/r)²= m r ω²
The distance r=(g.R2/w2)1/3
This equation shows that frequency of rotation of a satellite determine its distance4 from the earth’s surface.