ecpi.common.mission.attitude Module

Created on 16 mai 2018

@author: Colley Jean-Marc, APC/IN2P3/CNRS

Functions

compute_local_frame_on_sphere(p_ptg_radec[, deg]) Return base of tangent local frame of unit sphere for
direlev_to_xyz(p_direlev[, deg]) Convert spherical coordinate with CNES convention to unit cartesian vector
ptgori_to_quaternion(p_ptg_radec, p_ori[, deg]) Compute quaternion associated to rotation defined by a pointing direction and orientation
xyz_to_direlev(p_xyz[, deg]) Convert unit cartesian vector in spherical coordinate with CNES convention

Classes

AttitudeECLAIRs([p_frame_cat, no_biais]) Attitude for ECLAIRs instrument
AttitudeMXT([p_frame_cat, no_biais]) Attitude for MXT instrument
AttitudeVT([p_frame_cat, no_biais]) Attitude for VT instrument

Class diagram

_images/classes_ecpi.common.mission.attitude.png