Orbit of Planets 2
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Complex Math
This example demonstrates the behavior of planetary orbits. It involves the concept of functions, particularly the parametric equations of orbits. Using GeoGebra commands such as Point, Segment, Polygon, Circle, and Intersect, you can dynamically observe the changes in planetary orbits. Suitable for high school mathematics education and learning.
GeoGebra Commands & Parameters
Point(b) → APoint(c) → BSegment(C, A) → dSegment(C, B) → fPoint(c) → DSegment(B, D) → iPoint(Circle[A, 1.4142135623730951]) → FSegment(A, F) → gSegment(A, F) → hPolygon(B, C, D) → poly1, d_1, b_1, c_1Segment(C, D) → d_hPoint(c) → EPoint(c) → GSegment(B, G) → τSegment(F, G) → nSlope(n) → mSlope(d_h) → m_1Circle(C, A) → kArea(k) → ePointIn(k) → PointkLine(H, f) → jIntersect(k, j, 2) → ISegment(C, I) → lLine(I, b) → pIntersect(p, d) → JSegment(C, J) → qSegment(J, I) → sPoint(s) → KSegment(C, K) → tSegment(I, F) → a_1Segment(J, A) → e_1Polygon(C, I, F, G, B) → poly2, c_2, i_1, f_1, g_1, b_2Name(o) → A1Name(u) → B1Name(a) → C1Point(k) → LCircle(M, N) → h_1Point(h_1) → OPoint(h_1) → PMidpoint(O, P) → QSegment(M, O) → j_1Segment(z_1, z_2) → k_1Vector(T, U) → vTranslate(z_1, v) → z_3Translate(z_2, v) → z_4Segment(z_3, z_4) → l_1Point(l_1) → VSegment(V, W) → n_1Segment(V, Z) → p_1Segment(V, A_1) → q_1Segment(V, B_1) → r_1Segment(V, C_1) → s_1Segment(V, D_1) → t_1Segment(V, E_1) → a_2Segment(V, F_1) → d_2Segment(V, G_1) → e_2Point(j_1) → H_1Circle(H_1, I_1) → f_2Circle(H_1, J_1) → g_2Circle(H_1, K_1) → h_2Circle(H_1, L_1) → k_2Circle(H_1, M_1) → p_2Circle(H_1, N_1) → q_2Circle(H_1, O_1) → r_2Point(h_1) → P_1Circle(H_1, P_1) → s_2Segment(V, Q_1) → i_2