This file summarises the convention used to describe the direction of flight
of the Venus Express spacecraft, especially in the NADIR pointing mode (see
VEX_POINTING_MODE_DESC.TXT).
Version 1.1
Written by Maud Barthelemy
21/07/2006
Modified by Maud Barthelemy
30/01/2007
Modified after ASPERA Peer review by Maud Barthelemy
23/02/2009
The SPACECRAFT_ORIENTATION element defines the Venus Express direction of
flight with respect to its spacecraft reference frame. The direction of flight
is given as a 3-tuple (x,y,z). The paragraph below describes how to derive the
(x,y,z) values.
When the spacecraft is in nadir pointing mode, the +Z axis points towards the
centre of Venus and the +X axis is perpendicular to the ground track. Unlike
Mars Express, the speed vector of the spacecraft can be tilted from the +Y
axis direction at an angle a. The 3-tuple (x, y, z) defines the coordinates of
the normalised spacecraft speed vector. As a consequence, we have:
x = sin a
y = cos a
Y ^
|
| ^
| / V
|a /
| /
|/_________> X
View of the spacecraft speed vector in the (X,Y) plane