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Fundamentals of astrodynamics and applications 4th Edition (2013)

Fundamentals of Astrodynamics and Applications has been a part of the Space Technology Library for over a decade now. I’m sure it will continue to be the standard reference in the field and to serve as an excellent introduction and fundamental resource for anyone working in astrodynamics.

Fundamentals of Astrodynamics and Applications has been a part of the Space Technology Library for over a decade now. I’m sure it will continue to be the standard reference in the field and to serve as an excellent introduction and fundamental resource for anyone working in astrodynamics.

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14 EQUATIONS OF MOTION 1.2

Directrix

l = p/e

p

r/e

r

r F F'

F'

n

F

r p

r p

/e

Figure 1-4. Geometry for Conic Sections. We create conic sections by recognizing that the

sum of the distance from both foci to any point on the orbit is constant. The ratio of

the distance from a focus to the orbit and the distance from that point to the directrix

is also a constant called the eccentricity, e. The closest point in the orbit to the primary

focus, F, is the radius of periapsis, r p

. The distance l is a standard quantity used

to describe conic sections.

simple means of creating an ellipse is to take a fixed-length string, two tacks, and a pencil

to stretch out the string and move on a blank page [See Fig. 1-4]. As the pencil

stretches the string and moves, the length from each focus changes, and the pencil traces

out the ellipse. Prussing and Conway (1993:62) show this mathematically for any point

on the conic section,

r F′ + r F = constant = 2a

(1-1)

r F – r F′ = constant = 2c

Each focus of a conic section has a corresponding stationary line called a directrix.

The ratio of the distance from a focus to a point on the orbit and the distance from that

point to the focus’ corresponding directrix is a constant defined as the eccentricity. The

eccentricity, e, is a fixed constant for each type of conic section; it indicates the orbit’s

shape—its “roundness” or “flatness.” The eccentricity is never negative, and its value

determines the type of conic section for common orbits. It’s unity for parabolic and rectilinear

orbits, less than unity for ellipses, zero for circles, and greater than unity for

hyperbolas. The eccentricity is

c

e = --

(1-2)

a

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