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

摘要

The satellite comprises: a first device (9) having a first operating law dependent on a first pointing angle (α1) of the first device with respect to a first target object; a second device (13) having a second operating law dependent on a second pointing angle (α2) of the second equipment with respect to a second target object. This method consists in optimizing an attitude of the satellite at each point (P) of the orbit (5), taking into account a first constraint corresponding to the first operating law and a second constraint corresponding to the second operating law.