MIT OpenCourseWare http://ocw.mit.edu 16.346 Astrodynamics Fall 2008 For information about citing these materials or our Terms of Use, visit: http://ocw.mit.edu/terms. Lecture 16 Non-Singular ``Gauss-Like'' Method for the BVP Derivation of the Time Equation Start with the Lagrange time equation and the equation for the mean point radius 3 1√ 2 2 µ(t2 − t1 ) = a (ψ − sin ψ cos φ) r0 = r0p = FS = a(1 − cos φ) = r0p (1 + tan2 12 ψ ) √ 1 1 r1 r2 cos 12 θ 2 2 (r1 + r2 ) + √ r1 r2 cos 12 θ (1) (2) (3) (4) Eliminate cos φ and compare with the elementary form of Kepler’s equation 1 µ r0 sin ψ − t ) = ψ − sin ψ + (t 2 1 E ⇐⇒ ψ 2 a3 a Identify q ⇐⇒ r0 q µ (t − τ ) = E − sin E + sin E 3 a a t − τ ⇐⇒ 12 (t2 − t1 ) since t2 − t1 = (t2 − τ ) + (τ − t1 ) = 2(t2 − τ ). Fig. 7.4 from An Introduction to the Mathematics and Methods of Astrodynamics. Courtesy of AIAA. Used with permission. From the classical relation between the true and eccentric anomalies: tan2 1 2 f= 1+e tan2 1−e 1 2 2a − q tan2 q E= where we have defined F S cos f = 0 = F0 P2 16.346 Astrodynamics x = tan2 1 2 1 2 E E and r1 r2 cos 21 θ 1 2 (r1 + r2 ) then 2 tan2 12 E q = a tan2 12 f + tan2 =⇒ = tan2 √ = 1 2 f . 1 2 E Since 1 − cos f F P − F0 S = 0 2 1 + cos f F0 P2 + F0 S Lecture 16 = 2x +x Relation to Gauss’ Classical Method The time equation 2 tan 12 E q q 1 µ q3 − t ) × = E − sin E + sin E = E − sin E + × (t 1 a3 a a 1 + tan2 12 E 2 q3 2 = sin E becomes 4 tan3 21 E 1 µ 8 3 1 − t ) × × tan E = E − sin E + (t 1 2 2 q3 2 ( + x)(1 + x) ( + x)3 Then, since q = r0 = r0p (1 + tan2 1 2 E ) = r0p (1 + x) we have an expression for the transfer time as a function only of E ≡ ψ : 4 tan3 12 E 4 tan3 12 E µ 3 = E − sin E + 3 (t2 − t1 ) × 8r0p ( + x)(1 + x) [( + x)(1 + x)] 2 E − sin E m m3 =m + 1 3 3 ( + x)(1 + x) [( + x)(1 + x)] 4 tan 2 E Following Gauss, we can define y as y2 = m ( + x)(1 + x) so that where µ(t2 − t1 )2 m= 3 8r0p y3 − y2 = m E − sin E 4 tan3 12 E √ r1 + r2 − 2 r1 r2 cos = √ r1 + r2 + 2 r1 r2 cos and 1 2 1 2 θ θ Note: The new y does not have the same geometric significance as Gauss’ y . Parameter and Semimajor Axis 1 2x 2xy 2 = = mr0p a r0p (1 + x)( + x) √ sin φ c c(1 + x)2 y 2 (1 + x)2 cy 2 (1 + x)2 p = = = = = pm 8ax 4mr0p sin ψ m 2a sin2 ψ r0p (1 + x) 2x q = = a +x a =⇒ where we have used the equation c = 2a sin ψ sin φ from Lecture 9, Page 1 16.346 Astrodynamics Lecture 16 Universal Form The equations are universal when x is extended to include the other conics: ⎧ ⎨ tan2 14 (E2 − E1 ) x= 0 ⎩ − tanh2 14 (H2 − H1 ) ellipse parabola hyperbola Comparing the Structure of Gauss’ Method and the New Method Gauss’ Method D≡ √ r1 r2 cos 12 θ √ r1 + r2 − 2 r1 r2 cos 12 θ = 4D 2 µ(t2 − t1 ) m= 8D3 2 1 x ≡ sin 2 ψ m y2 = +x 2ψ − sin 2ψ y3 − y2 = m sin3 ψ p cy 2 = pm 4mD 2y 2 x 1 = (1 − x) a mD 16.346 Astrodynamics New Method √ D ≡ 14 (r1 + r2 + 2 r1 r2 cos 12 θ) √ r1 + r2 − 2 r1 r2 cos 12 θ = 4D µ(t2 − t1 )2 m= 8D3 x ≡ tan2 12 ψ m y2 = ( + x)(1 + x) ψ − sin ψ y3 − y2 = m 4 tan3 12 ψ cy 2 p = (1 + x)2 pm 4mD 2y 2 x 1 = a mD Lecture 16