- •CONTENTS
- •Preface
- •To the Student
- •Diagnostic Tests
- •1.1 Four Ways to Represent a Function
- •1.2 Mathematical Models: A Catalog of Essential Functions
- •1.3 New Functions from Old Functions
- •1.4 Graphing Calculators and Computers
- •1.6 Inverse Functions and Logarithms
- •Review
- •2.1 The Tangent and Velocity Problems
- •2.2 The Limit of a Function
- •2.3 Calculating Limits Using the Limit Laws
- •2.4 The Precise Definition of a Limit
- •2.5 Continuity
- •2.6 Limits at Infinity; Horizontal Asymptotes
- •2.7 Derivatives and Rates of Change
- •Review
- •3.2 The Product and Quotient Rules
- •3.3 Derivatives of Trigonometric Functions
- •3.4 The Chain Rule
- •3.5 Implicit Differentiation
- •3.6 Derivatives of Logarithmic Functions
- •3.7 Rates of Change in the Natural and Social Sciences
- •3.8 Exponential Growth and Decay
- •3.9 Related Rates
- •3.10 Linear Approximations and Differentials
- •3.11 Hyperbolic Functions
- •Review
- •4.1 Maximum and Minimum Values
- •4.2 The Mean Value Theorem
- •4.3 How Derivatives Affect the Shape of a Graph
- •4.5 Summary of Curve Sketching
- •4.7 Optimization Problems
- •Review
- •5 INTEGRALS
- •5.1 Areas and Distances
- •5.2 The Definite Integral
- •5.3 The Fundamental Theorem of Calculus
- •5.4 Indefinite Integrals and the Net Change Theorem
- •5.5 The Substitution Rule
- •6.1 Areas between Curves
- •6.2 Volumes
- •6.3 Volumes by Cylindrical Shells
- •6.4 Work
- •6.5 Average Value of a Function
- •Review
- •7.1 Integration by Parts
- •7.2 Trigonometric Integrals
- •7.3 Trigonometric Substitution
- •7.4 Integration of Rational Functions by Partial Fractions
- •7.5 Strategy for Integration
- •7.6 Integration Using Tables and Computer Algebra Systems
- •7.7 Approximate Integration
- •7.8 Improper Integrals
- •Review
- •8.1 Arc Length
- •8.2 Area of a Surface of Revolution
- •8.3 Applications to Physics and Engineering
- •8.4 Applications to Economics and Biology
- •8.5 Probability
- •Review
- •9.1 Modeling with Differential Equations
- •9.2 Direction Fields and Euler’s Method
- •9.3 Separable Equations
- •9.4 Models for Population Growth
- •9.5 Linear Equations
- •9.6 Predator-Prey Systems
- •Review
- •10.1 Curves Defined by Parametric Equations
- •10.2 Calculus with Parametric Curves
- •10.3 Polar Coordinates
- •10.4 Areas and Lengths in Polar Coordinates
- •10.5 Conic Sections
- •10.6 Conic Sections in Polar Coordinates
- •Review
- •11.1 Sequences
- •11.2 Series
- •11.3 The Integral Test and Estimates of Sums
- •11.4 The Comparison Tests
- •11.5 Alternating Series
- •11.6 Absolute Convergence and the Ratio and Root Tests
- •11.7 Strategy for Testing Series
- •11.8 Power Series
- •11.9 Representations of Functions as Power Series
- •11.10 Taylor and Maclaurin Series
- •11.11 Applications of Taylor Polynomials
- •Review
- •APPENDIXES
- •A Numbers, Inequalities, and Absolute Values
- •B Coordinate Geometry and Lines
- •E Sigma Notation
- •F Proofs of Theorems
- •G The Logarithm Defined as an Integral
- •INDEX
662 |||| CHAPTER 10 PARAMETRIC EQUATIONS AND POLAR COORDINATES
and the length of the minor axis is 1.14 1010 km. Use Simpson’s Rule with n 10 to estimate the distance traveled by the planet during one complete orbit around the sun.
61.Find the area of the region enclosed by the hyperbola
x2 a 2 y 2 b 2 1 and the vertical line through a focus.
62.(a) If an ellipse is rotated about its major axis, find the volume of the resulting solid.
(b)If it is rotated about its minor axis, find the resulting volume.
63.Let P1 x1, y1 be a point on the ellipse x 2 a 2 y 2 b 2 1 with
foci F1 and F2 and let and be the angles between the lines PF1, PF2 and the ellipse as shown in the figure. Prove that
. This explains how whispering galleries and lithotripsy work. Sound coming from one focus is reflected and passes through the other focus. [Hint: Use the formula in Problem 17 on page 268 to show that tan tan .]
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64. Let P x1, y1 be a point on the hyperbola x 2 a 2 y 2 b 2 1 with foci F1 and F2 and let and be the angles between the lines PF1, PF2 and the hyperbola as shown in the figure. Prove that . (This is the reflection property of the hyperbola. It shows that light aimed at a focus F2 of a hyperbolic mirror is reflected toward the other focus F1.)
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10.6CONIC SECTIONS IN POLAR COORDINATES
In the preceding section we defined the parabola in terms of a focus and directrix, but we defined the ellipse and hyperbola in terms of two foci. In this section we give a more unified treatment of all three types of conic sections in terms of a focus and directrix. Furthermore, if we place the focus at the origin, then a conic section has a simple polar equation, which provides a convenient description of the motion of planets, satellites, and comets.
1 THEOREM Let F be a fixed point (called the focus) and l be a fixed line (called the directrix) in a plane. Let e be a fixed positive number (called the eccentricity). The set of all points P in the plane such that
PF e
Pl
(that is, the ratio of the distance from F to the distance from l is the constant e) is a conic section. The conic is
(a)an ellipse if e 1
(b)a parabola if e 1
(c)a hyperbola if e 1
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SECTION 10.6 CONIC SECTIONS IN POLAR COORDINATES |||| 663
PROOF Notice that if the eccentricity is e 1, then PF Pl and so the given condition simply becomes the definition of a parabola as given in Section 10.5.
Let us place the focus F at the origin and the directrix parallel to the y-axis and
d units to the right. Thus the directrix has equation x d and is perpendicular to the polar axis. If the point P has polar coordinates r, , we see from Figure 1 that
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Pl d r cos |
Thus the condition PF Pl e, or PF e Pl , becomes
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r e d r cos |
If we square both sides of this polar equation and convert to rectangular coordinates, we get
x2 y2 e2 d x 2 e2 d2 2dx x2
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If e 1, then 1 e2 0 and we see that Equation 3 represents a hyperbola. Just as we did before, we could rewrite Equation 3 in the form
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664 |||| CHAPTER 10 PARAMETRIC EQUATIONS AND POLAR COORDINATES
By solving Equation 2 for r, we see that the polar equation of the conic shown in Figure 1 can be written as
r 1
ed
e cos
If the directrix is chosen to be to the left of the focus as x d, or if the directrix is chosen to be parallel to the polar axis as y d, then the polar equation of the conic is given by the following theorem, which is illustrated by Figure 2. (See Exercises 21–23.)
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FIGURE 2 |
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6 THEOREM A polar equation of the form |
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represents a conic section with eccentricity e. The conic is an ellipse if e 1, |
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V EXAMPLE 1 Find a polar equation for a parabola that has its focus at the origin and whose directrix is the line y 6.
SOLUTION Using Theorem 6 with e 1 and d 6, and using part (d) of Figure 2, we see that the equation of the parabola is
6
r 1 sin
V EXAMPLE 2 A conic is given by the polar equation
10
r 3 2 cos
Find the eccentricity, identify the conic, locate the directrix, and sketch the conic.
SOLUTION Dividing numerator and denominator by 3, we write the equation as
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FIGURE 3 |
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SECTION 10.6 CONIC SECTIONS IN POLAR COORDINATES |||| 665
From Theorem 6 we see that this represents an ellipse with e 23 . Since ed 103 , we have
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so the directrix has Cartesian equation x 5. When 0, r 10; when , |
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FIGURE 4
12 r=2+4sin ¨
11
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10 r=3-2 cos ¨
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FIGURE 5
EXAMPLE 3 Sketch the conic r |
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SOLUTION Writing the equation in the form |
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we see that the eccentricity is e 2 and the equation therefore represents a hyperbola. Since ed 6, d 3 and the directrix has equation y 3. The vertices occur when
2 and 3 2, so they are 2, 2 and 6, 3 2 6, 2 . It is also useful to plot the x-intercepts. These occur when 0, ; in both cases r 6. For additional accuracy we could draw the asymptotes. Note that r l when 1 2 sin l 0 or 0 and 1 2 sin 0 when sin 12 . Thus the asymptotes are parallel to the rays
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When rotating conic sections, we find it much more convenient to use polar equations
than Cartesian equations. We just use the fact (see Exercise 77 in Section 10.3) that the |
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EXAMPLE 4 |
If the ellipse of Example 2 is rotated through an angle |
4 about the |
origin, find a polar equation and graph the resulting ellipse. |
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SOLUTION We get the equation of the rotated ellipse by replacing with 4 in the equation given in Example 2. So the new equation is
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3 2 cos 4 |
We use this equation to graph the rotated ellipse in Figure 5. Notice that the ellipse has |
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M |
666 |||| CHAPTER 10 PARAMETRIC EQUATIONS AND POLAR COORDINATES
In Figure 6 we use a computer to sketch a number of conics to demonstrate the effect of varying the eccentricity e. Notice that when e is close to 0 the ellipse is nearly circular, whereas it becomes more elongated as e l 1 . When e 1, of course, the conic is a parabola.
e=0.1 |
e=0.5 |
e=0.68 |
e=0.86 |
e=0.96 |
e=1 |
e=1.1 |
e=1.4 |
e=4 |
FIGURE 6
KEPLER’S LAWS
In 1609 the German mathematician and astronomer Johannes Kepler, on the basis of huge amounts of astronomical data, published the following three laws of planetary motion.
KEPLER’S LAWS
1.A planet revolves around the sun in an elliptical orbit with the sun at one focus.
2.The line joining the sun to a planet sweeps out equal areas in equal times.
3.The square of the period of revolution of a planet is proportional to the cube of the length of the major axis of its orbit.
Although Kepler formulated his laws in terms of the motion of planets around the sun, they apply equally well to the motion of moons, comets, satellites, and other bodies that orbit subject to a single gravitational force. In Section 13.4 we will show how to deduce Kepler’s Laws from Newton’s Laws. Here we use Kepler’s First Law, together with the polar equation of an ellipse, to calculate quantities of interest in astronomy.
For purposes of astronomical calculations, it’s useful to express the equation of an ellipse in terms of its eccentricity e and its semimajor axis a. We can write the distance d from the focus to the directrix in terms of a if we use (4):
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So ed a 1 e2 . If the directrix is x d,
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then the polar equation is
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planet
r
¨
sun
aphelion perihelion
FIGURE 7
SECTION 10.6 CONIC SECTIONS IN POLAR COORDINATES |||| 667
7 The polar equation of an ellipse with focus at the origin, semimajor axis a, eccentricity e, and directrix x d can be written in the form
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1 e cos |
The positions of a planet that are closest to and farthest from the sun are called its perihelion and aphelion, respectively, and correspond to the vertices of the ellipse. (See Figure 7.) The distances from the sun to the perihelion and aphelion are called the perihelion distance and aphelion distance, respectively. In Figure 1 the sun is at the focus F,
so at perihelion we have 0 and, from Equation 7, |
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8 The perihelion distance from a planet to the sun is a 1 e and the aphelion distance is a 1 e .
EXAMPLE 5
(a)Find an approximate polar equation for the elliptical orbit of the earth around the sun (at one focus) given that the eccentricity is about 0.017 and the length of the major axis is about 2.99 108 km.
(b)Find the distance from the earth to the sun at perihelion and at aphelion.
SOLUTION
(a) The length of the major axis is 2a 2.99 108, so a 1.495 108. We are given that e 0.017 and so, from Equation 7, an equation of the earth’s orbit around the sun is
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1 e cos |
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(b) From (8), the perihelion distance from the earth to the sun is
a 1 e 1.495 108 1 0.017 1.47 108 km
and the aphelion distance is
a 1 e 1.495 108 1 0.017 1.52 108 km |
M |
668 |||| CHAPTER 10 PARAMETRIC EQUATIONS AND POLAR COORDINATES
10.6E X E R C I S E S
1– 8 Write a polar equation of a conic with the focus at the origin and the given data.
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Hyperbola, |
eccentricity 47, |
directrix y 6 |
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9–16 (a) Find the eccentricity, (b) identify the conic, (c) give an equation of the directrix, and (d) sketch the conic.
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r |
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8 |
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6 |
2 cos |
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5 sin |
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r |
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3 |
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16. |
r |
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4 |
8 cos |
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6 sin |
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;17. |
(a) Find the eccentricity and directrix of the conic |
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r 1 1 2 sin and graph the conic and its directrix.
(b)If this conic is rotated counterclockwise about the origin through an angle 3 4, write the resulting equation and graph its curve.
;18. Graph the conic r 4 5 6 cos and its directrix. Also graph the conic obtained by rotating this curve about the ori-
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gin through an angle 3. |
;19. |
Graph the conics r e 1 e cos with e 0.4, 0.6, |
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0.8, and 1.0 on a common screen. How does the value of e |
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affect the shape of the curve? |
;20. |
(a) Graph the conics r ed 1 e sin for e 1 and var- |
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ious values of d. How does the value of d affect the shape |
of the conic?
(b) Graph these conics for d 1 and various values of e. How does the value of e affect the shape of the conic?
21.Show that a conic with focus at the origin, eccentricity e, and directrix x d has polar equation
r |
ed |
1 e cos |
22.Show that a conic with focus at the origin, eccentricity e, and directrix y d has polar equation
r |
ed |
1 e sin |
23.Show that a conic with focus at the origin, eccentricity e, and directrix y d has polar equation
r |
ed |
1 e sin |
24.Show that the parabolas r c 1 cos and r d 1 cos intersect at right angles.
25.The orbit of Mars around the sun is an ellipse with eccentricity 0.093 and semimajor axis 2.28 108 km. Find a polar equation for the orbit.
26.Jupiter’s orbit has eccentricity 0.048 and the length of the major axis is 1.56 109 km. Find a polar equation for the orbit.
27.The orbit of Halley’s comet, last seen in 1986 and due to return in 2062, is an ellipse with eccentricity 0.97 and one focus at the sun. The length of its major axis is 36.18 AU. [An astronomical unit (AU) is the mean distance between the earth and the sun, about 93 million miles.] Find a polar equation for the orbit of Halley’s comet. What is the maximum distance from the comet to the sun?
28.The Hale-Bopp comet, discovered in 1995, has an elliptical orbit with eccentricity 0.9951 and the length of the major axis is 356.5 AU. Find a polar equation for the orbit of this comet. How close to the sun does it come?
29.The planet Mercury travels in an elliptical orbit with eccentricity 0.206. Its minimum distance from the sun is
4.6107 km. Find its maximum distance from the sun.
30.The distance from the planet Pluto to the sun is
4.43109 km at perihelion and 7.37 109 km at aphelion. Find the eccentricity of Pluto’s orbit.
31.Using the data from Exercise 29, find the distance traveled by the planet Mercury during one complete orbit around the sun. (If your calculator or computer algebra system evaluates definite integrals, use it. Otherwise, use Simpson’s Rule.)