3. The time equation for elliptic orbits has the form M -Esino where: M is known as the mean anomaly, ø(in radians) is known

numerical methods with programming

3. The time equation for elliptic orbits has the form M -Esino where: M is known as the mean anomaly, ø(in radians) is known as the eccentric anomaly and E (between 0 and 1) is the eccentricity of the elliptic orbit. For a given value of E and for a given value of M in the range n M(n1) the solution for behaves as follows: M when is an even integer; M when n is an odd integer Solve for by the methods listed. The incremental search method (E 0.12, M 5.6) b. The fixed-point iteration method (E 0.12, M 5.6) c. The bisection method (E 0.23, M 5.6) d. The false position method (E = 0.23, M 5.6) The Newton, Raphson method (E 0.23, M 7.8) f. The secant method (E 0.23, M- 7.8 a. e.



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