METHOD FOR DETERMINING A PROFILE OF ATTITUDES OF A SATELLITE; COMPUTER PROGRAM PRODUCT

摘要

The planet gear comprises: a first equipment (9) having a first functioning law dependent on a first laying angle (α1) of the first equipment with respect to a first object of the target; a second equipment (13) with a second law of operation dependent on a second laying angle (α2) of the second piece of equipment with respect to a second object of the target. This method consists in optimizing a satellite attitude at each point (p) of the orbit (5), in view of a first stress corresponding to the first law of operation and to a second stress corresponding to the second law of operation.