| 摘要 |
<p>A tail fin assembly for a munition (12) having a housing configured for attachment to the munition (12), at least one flight control surface (418), an actuator (412) for effecting movement of the flight control surface(s) (418), so as to facilitate guiding of the munition (12), and a guidance system (402) for controlling the actuator mechanism (412). The guidance system has a global positioning system (GPS) receiver (416) for effecting control of the actuator mechanism (412).</p> |
