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Lambert's problem : ウィキペディア英語版
Lambert's problem
In celestial mechanics Lambert's problem is concerned with the determination of an orbit from two position vectors and the time of flight, solved by Johann Heinrich Lambert. It has important applications in the areas of rendezvous, targeting, guidance, and preliminary orbit determination.〔E. R. Lancaster & R. C. Blanchard, (''A Unified Form of Lambert’s Theorem'' ), Goddard Space Flight Center, 1968〕 Suppose a body under the influence of a central gravitational force is observed to travel from point ''P1'' on its conic trajectory, to a point ''P2'' in a time ''T''. The time of flight is related to other variables by Lambert’s theorem, which states:
:''The transfer time of a body moving between two points on a conic trajectory is a function only of the sum of the distances of the two points from the origin of the force, the linear distance between the points, and the semimajor axis of the conic.''〔James F. Jordon, (''The Application of Lambert’s Theorem to the Solution of Interplanetary Transfer Problems'' ), Jet Propulsion Laboratory, 1964〕
Stated another way, Lambert's problem is the boundary value problem for the differential equation
: \ddot = -\mu \cdot \frac \ \
of the two-body problem for which the Kepler orbit is the general solution.
The precise formulation of Lambert's problem is as follows:
Two different times \ t_1 \ ,\ t_2\ and two position vectors \bar r_1 = r_1 _1 ,\ \bar r_2 = r_2 _2\ are given.
Find the solution \bar r(t) satisfying the differential equation above for which
: \bar r(t_1)=\bar r_1
: \bar r(t_2)=\bar r_2.
==Initial geometrical analysis==

The three points
; F_1 \ : The centre of attraction
; P_1 \ : The point corresponding to vector \bar r_1\
; P_2 \ : The point corresponding to vector \bar r_2\
form a triangle in the plane defined by the vectors \bar r_1\ and \bar r_2\ as illustrated in figure 1. The distance between the points P_1 \ and P_2 \ is 2d \ , the distance between the points P_1 \ and F_1 \ is r_1 = r_m-A \ and the distance between the points P_2 \ and F_1 \ is r_2 = r_m+A \ . The value A \ is positive or negative depending on which of the points P_1 \ and P_2 \ that is furthest away from the point F_1 \ . The geometrical problem to solve is to find all ellipses that go through the points P_1 \ and P_2 \ and have a focus at the point F_1 \
The points F_1 \ , P_1 \ and P_2 \ define a hyperbola going through the point F_1 \ with foci at the points P_1 \ and P_2 \ . The point F_1 \ is either on the left or on the right branch of the hyperbola depending on the sign of A \ . The semi-major axis of this hyperbola is |A| \ and the eccentricity E\ is \frac\ . This hyperbola is illustrated in figure 2.
Relative the usual canonical coordinate system defined by the major and minor axis of the hyperbola its equation is
:\frac - \frac = 1 \quad (1)
with
:B = |A| \sqrt = \sqrt \quad (2)
For any point on the same branch of the hyperbola as F_1 \ the difference between the distances r_2 \ to point P_2 \ and r_1 \ to point P_1 \ is
r_2 - r_1 = 2A \quad (3)
For any point F_2 \ on the other branch of the hyperbola corresponding relation is
s_1 - s_2 = 2A \quad (4)
i.e.
:r_1 + s_1 = r_2 + s_2 \quad (5)
But this means that the points P_1 \ and P_2 \ both are on the ellipse having the focal points F_1 \ and F_2 \ and the semi-major axis
:a = \frac = \frac \quad (6)
The ellipse corresponding to an arbitrary selected point F_2 \ is displayed in figure 3.

抄文引用元・出典: フリー百科事典『 ウィキペディア(Wikipedia)
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