Exercises
1.
Transform the point into xy-coordinates.
2.
Transform the point into polar coordinates.
Use a polar grid to sketch the graph of the following polar
functions. Compare your sketch to the plot produced by the ''polar plotting
tool'' in the ''Tools'' section.
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3. | r = 5, q
= p/4 | | 4. | r =
-2, q = p/3 |
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Use a polar grid to sketch the graph of the following polar functions. Then
find the velocity vector v(q) at the given q.
Compare your sketch to the plot produced by the "polar plotting tool" in the
"Tools" section.
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21. |
x2 + y2 = 2y + 3 | |
22. | x2+y2 = 4x+2y |
23. | (x-1)2 + y2
= 4 | |
24. | x2+y2 = (x+y)2 |
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Identify the eccentricity and the parameter of the following ellipses. Also, find the
foci, the
semi-major axis, and the semi-minor axis. Then sketch the graph of the
ellipse.
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33. | foci at (0,0) and (6,0) |
| 34. | foci at (0,0) and (0,10) |
| semi-major axis of 5 |
| | semi-major axis of 13 |
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35. Show that a polar function of the form
is a parabola. What is its vertex?
36. Which curve in the xy-plane is represented by the polar
equation r = sec(q) tan(q) ?
37. Show that
38. Show that if r and q are functions of t and r(t) =
á r cos(q), r sin(q)
ñ , then
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d
dt
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er = eq |
dq
dt
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and |
d
dt
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eq = -er |
dq
dt
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39. Show that if r and q are functions of t and r( t) =
á rcos( q) ,rsin( q)
ñ , then
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æ è
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d2r
dt2
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-r |
æ è
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dq
dt
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ö ø
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2
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ö ø
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er + |
æ è
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2 |
dr
dt
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dq
dt
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+r |
d2q
dt2
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ö ø
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eq |
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(Hint: See exercise 38).
40. Show that y = mx+b is pulled back into polar coordinates to the
function
At what value of q does r not exist? What is significant about
this value of q?
41. The orbit of the earth about the sun is an ellipse with the
sun's center as one focus. The parameter of the earth's orbit is 185,740,000 miles and the eccentricity is 0.017. What is the semi-major
axis, the semi-minor axis, and the foci of the earth's orbit.
42. A satellite has an orbit with a parameter of 4335 miles and
an eccentricity of 0.067. If we assume the earth is a sphere with a radius
of 3963 miles, what is the closest the satellite comes to the earth?
43. The positions of a planet closest to and farthest from the sun
are called its perihelion and aphelion, respectively.
Show that if 0 < e < 1 and if the planet's orbit is given by
then the perihelion distance is a( 1-e) and the
aphelion distance is a( 1+e) .
44. Pluto is at a distance of 4.43×109 km when it is
closest to the Sun and is at a distance 7.37×109 km when it is
farthest from the sun. Use the result in exercise 39 to determine the
eccentricity of the orbit.
45. Write to Learn: Write a short essay in which you derive and explain
the following identities:
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e = |
r(0) - r(p)
r(0)
+ r(p)
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46. The Eccentric Anomaly: The equation in polar
coordinates of an ellipse centered on the negative x-axis is
Let a = p/( 1-e2) and let k = p/(1+e) . The auxiliary circle of the ellipse is the
circle centered at ( k-a,0) with radius a, and the eccentric anomaly of an ellipse is the angle E formed with by the radius a of the circle that terminates on the vertical line through the point P( r,q) (see figure below):
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click image to toggle to an animation |
(animation created by Clayton Clark) |
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The eccentric anomaly is important in celestial mechanics, where we often
reparameterize r as a function of the angle E.
- Show that r cos( q) = a cos( E) - ae (hint: in the figure above, rcos( p-q) > 0 and acos( E) > 0).
- Use (a) and the fact that r + ercos(q) = p to show that
- Show that p = a( 1-e2) , so that (b) implies
that
- Use the definition of k to show that ae = a-k and that
(c) can be written in the form
- Explain why the segment BP in the figure above has a length of
| BP| = ( a-k) | cos( E)| |
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How might (4) and the length of BP be used to suggest a
different method for constructing an ellipse?