#G07 · Geometry & Trigonometry · Lv.2View in 3D Mind-Map
Conic Sections (Parabola, Ellipse, Hyperbola)
Apollonius & Johannes Kepler · 200 BCE
Algebraic equations of curves formed by slicing a cone—governing Keplerian planetary/satellite orbits, parabolic dish antennas, and quadratic optimization contours.
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Semi-major a
Semi-minor b
Eccentricity e
0.8000
Focal Distance ±c
±4.000
Ellipse Area πab
47.12
Prerequisite Path (7 STEP)
Full Path AnalyzerClick steps in order to follow the 3D neon path from basics to target.
STEP 1#A01Linear Equation & Balance Axiom
STEP 2#A02Polynomial Expansion & Factoring
STEP 3#A03Laws of Exponents & Radicals
STEP 4#G01Pythagorean Theorem
STEP 5#A04Quadratic Formula & Discriminant
STEP 6#G022D/3D Euclidean Distance Formula
STEP 7#G07Conic Sections (Parabola, Ellipse, Hyperbola)
🚀 Next Unlocks (Derived Formulas) (2)
Geometric & Intuitive Insight
두 초점 F, F' 으로부터의 거리 합이 2a로 일정한 점들의 자취가 타원입니다. 두 초점이 하나로 합쳐지면(이심률 e=0) 완벽한 원이 됩니다.
Step-by-Step Derivation
- Step 1.1단계: 두 초점 F(c, 0), F'(-c, 0) 으로부터 거리의 합이 2a 인 점 P(x, y) 의 방정식을 세웁니다.
- Step 2.2단계: √((x-c)² + y²) + √((x+c)² + y²) = 2a 의 양변을 제곱하여 근호를 정리합니다.
- Step 3.3단계: b² = a² - c² 으로 치환하면 x²/a² + y²/b² = 1 표준형 방정식이 도출됩니다.
AI & Coding Real-World Use
Kepler satellite orbit simulation and Multivariate Gaussian covariance ellipses in ML
#Kepler Orbit Sim#Mahalanobis Ellipse#Antenna Optics
const eccentricity = (a: number, b: number) => Math.sqrt(1 - (b*b)/(a*a));Geometry & Trigonometry — Related Formulas in This Cluster
Pythagorean Theorem
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