Space vehicle e.g. satellite piloting process, involves controlling direction of space vehicle to orient wind mill axis with respect to time for creating moment around inertial mark direction

摘要

The process involves creating two moments changing orientation of a space vehicle e.g. satellite (10) around an wind mill axis (J) that is orthogonal to wings (16a,16b) mean plane and a unbalanced axis of wings nominal plane by misaligning the wings in opposite and same directions, respectively. The vehicle direction is controlled to orient the windmill axis with respect to time to create a moment around an inertial mark direction.