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