The method involves determining mean biases of accelerometers and gyrometers of an inertial unit (IM) of a craft (M) using an inertial unit (IL) of a carrier (L) before firing the craft from the carrier. Measurements of the accelerometers and the gyrometer...

Systems and methods to incorporate master navigation system resets during transfer alignment are provided. In one embodiment, a system comprises: a set of local inertial sensors; a local navigation processor coupled to local inertial sensors, the local nav...