This paper provides a functional description of the navigation and guidance system in the Advanced Cruise Missile (ACM), one of the Air Force's newest stealth missiles. It also discusses some of the areas of improvement over the Air Launched Cruise Missile (ALCM). The Kalman Filter design accommodates velocity updates, including lateral velocities, and a nominal number of position updates from terrain correlation matching (TERCOM) to achieve a high accuracy, long range mission.<>
Advanced Cruise Missile guidance system description
1993-01-01
447811 byte
Conference paper
Electronic Resource
English
Computer guidance for the cruise missile
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