Kinematic synthesis of the spacecrafts programmed attitude motion at the Earth optic-electronic survey

Methods of calculating the spacecraft programmed attitude motion for three variants of optic-electronic survey by the Earth surface, are presented, namely: survey with alignment of an image motion lengthwise velocity into focal plane of orbital telescope, survey with coinciding the line-of-sight trace on the Earth surface with geodesic line and survey with fixed position of the telescope line-of-sight in orbital reference frame. Some results are represented which were obtained by elaborated software.