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) |
Return base of tangent local frame of unit sphere for |
direlev_to_xyz(p_direlev) |
Convert spherical coordinate with CNES convention to unit cartesian vector |
ptgori_to_quaternion(p_ptg_radec, p_ori) |
Compute quaternion associated to rotation defined by a pointing direction and orientation |
xyz_to_direlev(p_xyz) |
Convert unit cartesian vector in spherical coordinate with CNES convention |
xyz_to_thetaphi(p_xyz) |
Convert unit cartesian vector to physical spherical coordinate convention |
Classes¶
AttitudeECLAIRs([p_frame_cat]) |
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AttitudeMXT([p_frame_cat]) |
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AttitudeVT([p_frame_cat]) |
doc CNES 6.1.1 inertial reference frame |
SVOMPointingError |