3.4.6Conic Sections

Kepler's connection — orbits are ellipses (motivation)

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WHY should a maths student care?

WHAT we are doing: connecting the pure-geometry object (ellipse) to a physical law of motion.

WHY it matters: the ellipse's focus is normally an abstract point that makes distances behave nicely (r1+r2=constr_1+r_2 = \text{const}). Kepler's law tells us that this abstract point is physically special — it's where the gravitating mass lives. So the same ee (eccentricity), aa (semi-major axis) you compute in a conic problem literally describe a planet's orbit.

HOW it links: A body moving under an inverse-square attractive force (F1/r2F \propto 1/r^2) must follow a conic. Which conic depends on how much energy it has — this single fact unifies circles, ellipses, parabolas and hyperbolas as one family.


Kepler's three laws (the motivation)

Figure — Kepler's connection — orbits are ellipses (motivation)

Deriving the ellipse's key numbers from scratch

We won't do the full calculus orbit derivation (that's physics), but we derive the geometry that Kepler's first law needs, purely from the focus definition.

Step 1 — Set up the ellipse

x2a2+y2b2=1,a>b>0\frac{x^2}{a^2} + \frac{y^2}{b^2} = 1, \qquad a>b>0

  • Why? This is the standard ellipse centred at origin. aa = semi-major axis, bb = semi-minor.

The foci lie on the major axis at (±c,0)(\pm c, 0) where c=ae,e=eccentricity,b2=a2(1e2).c = ae, \qquad e = \text{eccentricity}, \qquad b^2 = a^2(1-e^2).

  • Why b2=a2(1e2)b^2 = a^2(1-e^2)? Take the point (0,b)(0,b) on the top of the ellipse. Its distances to the two foci are equal (by symmetry), each c2+b2\sqrt{c^2+b^2}. The sum-of-distances constant equals 2a2a, so each distance is aa. Thus c2+b2=a2c^2 + b^2 = a^2, giving b2=a2c2=a2(ae)2=a2(1e2)b^2 = a^2 - c^2 = a^2 - (ae)^2 = a^2(1-e^2). ✅

Step 2 — Nearest and farthest points (perihelion & aphelion)

Put the Sun at focus F1=(c,0)=(ae,0)F_1 = (c,0) = (ae,0). The planet's distance to the Sun along the major axis:

rmin=ac=a(1e)(perihelion, nearest)r_{\min} = a - c = a(1-e) \quad(\text{perihelion, nearest}) rmax=a+c=a(1+e)(aphelion, farthest)r_{\max} = a + c = a(1+e) \quad(\text{aphelion, farthest})

  • Why this step? The major-axis endpoints are at (±a,0)(\pm a, 0). Distance from (a,0)(a,0) to focus (ae,0)(ae,0) is aae=a(1e)a - ae = a(1-e); from (a,0)(-a,0) it is a+ae=a(1+e)a + ae = a(1+e). These are the closest/farthest a planet ever gets.

Step 3 — Why equal areas ⇒ faster near the Sun (Law 2 intuition)

The area swept per unit time is constant. Near perihelion the "radius arm" rr is short, so to sweep the same area the planet must swing through a bigger angle — i.e. move faster. This is angular-momentum conservation dressed as geometry.

dAdt=12r2dθdt=const\frac{dA}{dt} = \frac{1}{2} r^2\frac{d\theta}{dt} = \text{const}

  • Why? A thin triangle swept in time dtdt has area 12r(rdθ)\tfrac12 \cdot r \cdot (r\,d\theta). If dAdt\tfrac{dA}{dt} is constant and rr shrinks, dθdt\tfrac{d\theta}{dt} must grow.

Worked examples


Common mistakes (Steel-manned)


Active recall

Recall Cover and answer
  • Where does the Sun sit in a planet's elliptical orbit? → at one focus.
  • What is rminr_{\min} in terms of a,ea,e? → a(1e)a(1-e).
  • How do you get aa from perihelion and aphelion? → their average.
  • What does Kepler's 2nd law imply about speed? → faster near the Sun (equal areas).
  • State Kepler's 3rd law. → T2a3T^2 \propto a^3.
Recall Feynman: explain to a 12-year-old

Imagine tying a stone to a string and swinging it — but the string is stretchy gravity. The stone (planet) goes around the Sun, but not in a perfect circle: it makes a squashed loop called an ellipse. The Sun isn't in the middle of the squashed loop; it sits a little to one side, at a special spot called a focus. When the planet comes close to the Sun it speeds up (like a kid running faster around the tight corner of a track), and when it's far away it slows down. And here's the magic: if you know the closest and farthest distances, just average them and you get the "size" of the whole loop.


Flashcards

Kepler's 1st law states orbits are what shape, with Sun where?
Ellipses, with the Sun at one focus.
Perihelion distance in terms of a,ea,e?
rmin=a(1e)r_{\min}=a(1-e).
Aphelion distance in terms of a,ea,e?
rmax=a(1+e)r_{\max}=a(1+e).
How to recover semi-major axis from extreme distances?
a=12(rmin+rmax)a=\tfrac12(r_{\min}+r_{\max}).
Formula for eccentricity from extremes?
e=rmaxrminrmax+rmine=\dfrac{r_{\max}-r_{\min}}{r_{\max}+r_{\min}}.
Why b2=a2(1e2)b^2=a^2(1-e^2)?
Top point (0,b)(0,b) is distance aa from each focus, so c2+b2=a2c^2+b^2=a^2 with c=aec=ae.
Kepler's 2nd law in one word about speed?
Faster near the Sun (equal areas in equal times).
Kepler's 3rd law formula?
T2a3T^2\propto a^3.
Predict Mars period given a=1.524a=1.524 AU (Earth units)?
T=1.5243/21.88T=1.524^{3/2}\approx1.88 yr.
Is the Sun at the centre of the ellipse?
No — at a focus; centre is empty.
What kind of force produces conic orbits?
Inverse-square attractive force, F1/r2F\propto1/r^2.

Connections

Concept Map

forces motion along

energy selects

planet traces

Sun sits at

defined by

gives

located at

nearest point

farthest point

implies

relates

characterized by

Inverse-square force F ~ 1/r2

Conic orbit

Circle ellipse parabola hyperbola

Kepler Law 1 orbits

Ellipse

One focus F1

Sum of distances = 2a

b2 = a2 times 1-e2

c = ae

Perihelion a times 1-e

Aphelion a times 1+e

Kepler Law 2 areas

Faster near Sun

Kepler Law 3 periods

T2 ~ a3

e and a describe orbit

Hinglish (regional understanding)

Intuition Hinglish mein samjho

Dekho, conic section sirf geometry ki cheez nahi hai — nature khud ellipse banati hai! Kepler ne dekha ki har planet Sun ke around ek ellipse mein ghoomta hai, aur Sun ellipse ke centre pe nahi, balki ek focus pe baithta hai. Yahi reason hai ki focus itna important point hai jab hum conics padhte hain. Focus wahi jagah hai jahan "khinchne wala" body (Sun) hota hai.

Do khaas points yaad rakho: perihelion (Sun ke sabse paas, distance a(1e)a(1-e)) aur aphelion (sabse door, distance a(1+e)a(1+e)). Inn dono ka average nikaalo to aa (semi-major axis) mil jaata hai, aur inka difference-by-sum nikaalo to eccentricity ee mil jaati hai. Simple formulas, lekin poore orbit ki puri kahani inme chhupi hai.

Kepler ka doosra law kehta hai equal time mein equal area sweep hota hai — matlab Sun ke paas planet tez chalta hai, door jaake dheema. Socho jaise race track ke tight corner pe bacha fast bhaagta hai. Aur teesra law: T2a3T^2 \propto a^3 — bada orbit matlab lamba saal (Mars ka saal Earth se lamba). Yeh sab isliye important hai kyunki inverse-square gravity (F1/r2F \propto 1/r^2) wali koi bhi cheez conic hi banati hai — circle, ellipse, parabola, hyperbola sab ek hi family. Exam mein ellipse ke aa, bb, ee ke formulas ko iss physical picture se jodo, yaad rakhna aasaan ho jayega.

Go deeper — visual, from zero

Test yourself — Conic Sections

Connections