Methods for inductively transferring data and power to a plurality of guided projectiles to provide a lock-on-before-launch capability

摘要

Embodiments of an inductive power transfer method are generally described herein. In some embodiments, a method of transferring data and power to a plurality of guided projectiles located in launcher tubes on a helicopter is described herein. In some embodiments, power and data are inductively transferred across the launcher windings to the projectile windings to configure the control systems of the guided projectiles to provide a lock-on-before-launch capability.