Q2) Figure 3.5 shows the geometry of a planetary orbit around the sun. The position of the sun is given by S, the position of the planet is given by P. Let a denote the angle defined by PoOA, measured in radians. The dotted line is a circle concentric to the ellipse and having a radius equal to the major axis of the ellipse. Let T be the total period of the planet, and let t be the time required for the planet to go from A to P. Then Kepler's equation from orbital mechanics, relating x and t, is x-esinx= 2nt T Here is the eccentricity of the elliptical orbit (the extent to which it deviates from a circle). For an orbit of eccentricity = 0.01 (roughly equivalent to that of the Earth), what is the value of a corresponding to t= T/4? What is the value of a corresponding to t = T/8? Use Newton's method to solve the required equation. Figure 3.5 Orbital geometry for Problems 4 and 5

Advanced Engineering Mathematics
10th Edition
ISBN:9780470458365
Author:Erwin Kreyszig
Publisher:Erwin Kreyszig
Chapter2: Second-order Linear Odes
Section: Chapter Questions
Problem 1RQ
Question
Q2)
Figure 3.5 shows the geometry of a planetary orbit around the sun. The position of
the sun is given by S, the position of the planet is given by P. Let x denote the angle
defined by PoOA, measured in radians. The dotted line is a circle concentric to the
ellipse and having a radius equal to the major axis of the ellipse. Let T be the total
period of the planet, and let t be the time required for the planet to go from A to P.
Then Kepler's equation from orbital mechanics, relating x and t, is
x-esinx=
2πt
T
Here is the eccentricity of the elliptical orbit (the extent to which it deviates from
a circle). For an orbit of eccentricity = 0.01 (roughly equivalent to that of the
Earth), what is the value of x corresponding to t = T/4? What is the value of a
corresponding to t = T/8? Use Newton's method to solve the required equation.
Figure 3.5 Orbital geometry for Problems 4 and 5
Transcribed Image Text:Q2) Figure 3.5 shows the geometry of a planetary orbit around the sun. The position of the sun is given by S, the position of the planet is given by P. Let x denote the angle defined by PoOA, measured in radians. The dotted line is a circle concentric to the ellipse and having a radius equal to the major axis of the ellipse. Let T be the total period of the planet, and let t be the time required for the planet to go from A to P. Then Kepler's equation from orbital mechanics, relating x and t, is x-esinx= 2πt T Here is the eccentricity of the elliptical orbit (the extent to which it deviates from a circle). For an orbit of eccentricity = 0.01 (roughly equivalent to that of the Earth), what is the value of x corresponding to t = T/4? What is the value of a corresponding to t = T/8? Use Newton's method to solve the required equation. Figure 3.5 Orbital geometry for Problems 4 and 5
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