ecpi.common.mission.orbit Module
@author: BACON Philippe, APC/IN2P3/CNRS
Functions
direlev_to_xyz(p_direlev[, deg]) |
Convert spherical coordinate with CNES convention to unit cartesian vector |
earth_limb(position) |
Compute alpha limb angle |
norm(a[, ord, axis, keepdims, check_finite]) |
Matrix or vector norm. |
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 |
EclairsOrbit([orbit_filename, attitude_filename]) |
Manage orbital aspects for the SVOM mission. |
InstruECLAIRs([p_file_mask, p_nb_pix]) |
Implementation of the ECLAIRs mask geometry. |
Class diagram
