In this chapter, we'll work with orthonormal axes. We'll show how we can simplify the general equation of a conic section by means of a translation and a rotation. Further, we assume that the conic section is not degenerated.
We start from the general equation of a conic section.
F(x,y,1) =a x2 + 2 b" x y + a' y2 + 2 b' x + 2 b y + a" = 0
We start with translation of the axes to the point (xo,yo). The transformation formulas are
x = x' + xo y = y' + yo
In the new system of axes the equation is
a (x' + xo)2 + 2 b" (x' + xo) (y' + yo) + a' (y' + yo)2
+ 2 b' (x' + xo) + 2 b (y' + yo) + a" = 0
<=>
a x'2 + 2 b" x' y' + a' y'2 + 2(a xo + b" yo + b')x'
+ 2( b" xo + a' yo + b)y'+ a xo2 + 2 b" xo yo + a' yo2 + 2 b' xo + 2 b yo + a" = 0
To simplify this, we choose xo and yo such that
/ a xo + b" yo + b' = 0
\ b" xo + a' yo + b = 0
<=>
xo and yo is a solution of the system / Fx' (x,y,z) = 0 \ Fy' (x,y,z) = 0
Since delta is not zero, this system has always one unique solution.
With these special values of xo and yo, the equation of the conic section becomes
a x'2 + 2 b" x' y' + a' y'2 +
+ a xo + 2 b" xo yo + a' yo + 2 b' xo + 2 b yo + a" = 0
<=>
a x'2 + 2 b" x' y' + a' y'2 + F(xo,yo,1) = 0
Suppose the translation is done and then the equation of the conic section has the form
a x2 + 2 b" x y + a' y2 + a" = 0
To
reduce this further we use a rather tricky method.
(From a total different approach of the problem, this method is not tricky at
all. See later)
Consider the linear transformation of R x R with matrix
[a b"]
[b" a']
We
calculate the eigenvalues and characteristic vectors.
The eigenvalues are the roots of
|a - r b"|
|b" a' - r| = 0
<=>
(a - r)(a' - r) - b"b" = 0<=>
r2 -(a+a')r + aa' -b"2 = 0<=>
2 r -(a+a')r + delta = 0The
discriminant of this quadratic equation is never < 0. Say r1 and
r2 are these real roots. These roots are not 0 because their product
is not 0. Now we can calculate the characteristic vectors. We know that each
real multiple of such characteristic vector is also a characteristic vector.
So, it is possible to calculate a suitable characteristic vector such that this
vector is a unit vector.
Denote (cos(t),sin(t)) as coordinates of the characteristic unit vector
corresponding with r1. Then we have
[ a b"][cos(t)] [cos(t)]
[ b" a'][sin(t)] = r1 [sin(t)]
<=>
acos(t) + b"sin(t) = r1 cos(t) b"cos(t) + a'sin(t) = r1 sin(t)
Now we rotate the coordinate system by an angle = t. The transformation matrix is
[cos(t) -sin(t) 0]
M = [sin(t) cos(t) 0]
[ 0 0 1]
The new cubic matrix C1 of the conic section is given by the formula
TC1 = M C M
<=>
[cos(t) sin(t) 0][ a b" 0 ][cos(t) -sin(t) 0]
[-sin(t) cos(t) 0][ b" a' 0 ][sin(t) cos(t) 0]
[ 0 0 1][ 0 0 a"][ 0 0 1]
<=>
[cos(t) sin(t) 0][acos(t) + b"sin(t) -asin(t)+b"cos(t) 0 ]
[-sin(t) cos(t) 0][b"cos(t) + a'sin(t) -b"sin(t)+a'cos(t) 0 ]
[ 0 0 1][ 0 0 a"]
<=>
[cos(t) sin(t) 0][r1 cos(t) -asin(t)+b"cos(t) 0 ]
[-sin(t) cos(t) 0][r1 sin(t) -b"sin(t)+a'cos(t) 0 ]
[ 0 0 1][ 0 0 a"]
<=>
[r1 0 (*) 0 ]
[0 r2(*) 0 ]
[0 0 a"]
The elements marked by (*) are rather difficult to calculate. Here you see how it is done:
-a cos(t) sin(t) + b" cos2 (t) - b" sin2 (t) + a' sin(t) cos(t) = - sin(t) (a cos(t) + b" sin(t) ) + cos(t) (b" cos(t) + a' sin(t) ) = - sin(t) r1 cos(t) + cos(t) r1 sin(t) = 0and
a sin2 (t) - b" sin(t) cos(t) - b" sin(t) cos(t) + a' cos2 (t) = a(1 - cos2 (t)) - b"sin(t)cos(t) - b"sin(t) cos(t) + a'(1 - sin2 (t) ) = a + a' - (a cos2 (t) + b" sin(t)cos(t) + b"sin(t)cos(t) + a' sin2 (t)) = a + a' - (cos(t)(a cos(t) + b"sin(t))+ sin(t)(b"cos(t) + a'sin(t))) = a + a' - r1 = r1+ r2 - r1 = r2
The equation of the conic section in the new coordinate system is
r1 x'2 + r2 y'2 + a" = 0
This is the reduced equation of the conic section.
Take the conic section with equation
3 x2 + 2xy + 3 y2 -32 y + 92 = 0
We start with translation of the axes to the point (xo,yo).
xo and yo is a solution of the system / Fx' (x,y,z) = 0 \ Fy' (x,y,z) = 0<=>
/ 6 x + 2 y = 0 \ 2 x + 6 y = 32<=>
x = -2 and y = 6
After the translation the equation becomes
a x'2 + 2 b" x' y' + a' y'2 + F(xo,yo,1) = 0
<=>
3 x'2 + 2x'y' + 3 y'2 - 4 = 0
This is the equation of the conic section after the translation to (-2,4). Now we start with the rotation from the equation
3 x2 + 2xy + 3 y2 - 4 = 0
The eigenvalues are the roots of
|a - r b"|
|b" a' - r| = 0
<=>
|3-r 1|
| 1 3-r| = 0
<=>
r2 - 6 r + 8 = 0<=>
r1 = 4 and r2 = 2The equation of the conic section after the rotation is
r1 x'2 + r2 y'2 + a" = 0
<=>
4 x'2 + 2 y'2 - 4 = 0
<=>
x'2 y'2
----- + ----- = 11 2
and this is an ellipse
If you want to calculate the rotation angle t :
[ a b"][cos(t)] [cos(t)]
[ b" a'][sin(t)] = r1 [sin(t)]
<=>
acos(t) + b"sin(t) = r1cos(t) b"cos(t) + a'sin(t) = r1sin(t)<=>
3 cos(t) + sin(t) = 4 cos(t) cos(t) + 3 sin(t) = 4 sin(t)<=>
cos(t) - sin(t) = 0<=>
tan(t) = 1 choose t = pi/4
We start from the general equation of a conic section.
F(x,y,1) =a x2 + 2 b" x y + a' y2 + 2 b' x + 2 b y + a" = 0
Consider again the linear transformation of R x R with matrix
[a b"]
[b" a']
We calculate the eigenvalues and characteristic vectors. The eigenvalues are the roots of
|a - r b"|
|b" a' - r| = 0
<=>
(a - r)(a' - r) - b"b" = 0<=>
r2 -(a+a')r + aa' -b"2 = 0<=>
r2 -(a+a')r + delta = 0<=>
r2 -(a+a')r = 0<=>
r1 = 0 and r2 = a+a'
Denote (cos(t),sin(t)) as coordinates of the characteristic unit vector corresponding with r1=0. Then we have
[ a b"][cos(t)] [cos(t)]
[ b" a'][sin(t)] = r1 [sin(t)]
<=>
acos(t) + b"sin(t) = 0 b"cos(t) + a'sin(t) = 0
Now we rotate the coordinate system by an angle = t. The transformation matrix is
[cos(t) -sin(t) 0]
M = [sin(t) cos(t) 0]
[ 0 0 1]
The new cubic matrix C1 of the conic section is given by the formula
TC1 = M C M
In the same way as in the case delta not zero, you can show that
[0 0 * ]
C1 = [0 * * ]
[* * * ]
The
* stand for real numbers.
The equation of the conic section in the new coordinate system is of the form
a'y2 + 2 b' x + 2 b y + a" = 0
From this form we start with a translation
The equation of the conic section is
a'y2 + 2 b' x + 2 b y + a" = 0
If you calculate DELTA, you'll find
DELTA = - a' b'2
Since
the conic section is not degenerated, a' and b' are not zero.
We translate the axes to the point (xo,yo). The
transformation formulas are
x = x' + xo y = y' + yo
In the new system of axes the equation is
a'(y' + yo)2 + 2 b' (x' + xo) + 2 b (y' + yo) + a" = 0
<=>
a' y'2 + 2 b'x' + 2(a' yo + b)y' + a' yo 2 + 2 b' xo + 2 b yo + a" = 0
Because a' and b' are not zero, we can always choose xo and yo such that
a' yo + b = 0and
a' yo 2 + 2 b' xo + 2 b yo + a" = 0
then the reduced equation is
a' y'2 + 2 b'x' = 0
This is an equation of a parabola.
We start with the equation
9 x2 -24 xy + 16 y2 -2x + 4y + 5 = 0
delta
= 0.
One of the eigenvalues is r1 = 0.
Denote (cos(t),sin(t)) as coordinates of the unit characteristic vector
corresponding with r1=0. Then we have
[ a b"][cos(t)] [cos(t)]
[ b" a'][sin(t)] = r1 [sin(t)]
<=>
acos(t) + b"sin(t) = 0 b"cos(t) + a'sin(t) = 0<=>
9 cos(t) - 12 sin(t) = 0 -12 cos(t) + 16 sin(t) = 0then
tan(t) = 3/4 ; cos(t)= 4/5 ; sin(t) = 3/5[ 4/5 -3/5 0]
M = [ 3/5 4/5 0]
[ 0 0 1]
we find
T [ 0 0 2/5 ]
C1 = M C M = [ 0 25 11/5]
[2/5 11/5 5 ]
The equation after the rotation is
225 y + 4/5 x + 22/5 y + 5 = 0
Now the translation
x = x' + xo y = y' + yo4 22
25 (y'+ yo)2 + - (x'+ xo) + -- (y'+ yo) + 5 = 0
5 5
<=>
25y'2 + (4/5)x' + (50yo + 22/5)y' + 25yo2 + (4/5)xo + (22/5)yo + 5=0We choose xo and yo such that
(50yo + 22/5) = 0 and 25yo2 + (4/5)xo + (22/5)yo + 5=0
We find
751 11
xo = - ---- yo = - ----
125 125
The reduced equation is
25 y2 + (4/5) x = 0
Take a arbitrary conic section.
a x2 + 2 b" x y + a' y2 + 2 b' x z + 2 b y z + a" z2 = 0
The ideal points of that conic section are the solutions of
/|a x2 + 2 b" x y + a' y2 + 2 b' x z + 2 b y z + a" z2 = 0
| \ z = 0<=>
/| a x2 + 2 b" x y + a' y2 = 0
|\ z = 0
We see that the ideal points of the given conic section are the same points as these of the lines
a x2 + 2 b" x y + a' y2 = 0
From the theory about degenerated affine conic sections, we know the relationship between the nature and number of the ideal points and delta. So, about the given general conic section, we can say: