Accession Number : ADD006478

Title :   Trajectory Shaping of Anti-Armor Missiles via Tri-Mode Guidance.

Descriptive Note : Patent Application,

Corporate Author : DEPARTMENT OF THE ARMY WASHINGTON DC

Personal Author(s) : Yates ,Robert E ; Leonard ,John P ; Alongi ,Robert E ; Albanes ,Wilfredo V ; Bishop,Charles M

Report Date : 27 Apr 1979

Pagination or Media Count : 11

Abstract : In a missile system, a simple way to guide a missile in a predetermined trajectory from launch to the impacting with a target for optimum warhead penetration of armor by a guided missile. Initially, the missile is guided in yaw by proportional navigation. Subsequently it is guided in pitch first by a pitch programmer until the missile reaches a predetermined gimbal angle between a line of sight of a seeker of the missile and a centerline of the missile, then in pitch by a pseudo-time-optimal closed loop controller to direct the missile pitch attitude at a predetermined rate toward a target until said missile reaches another predetermined gimbal angle, and finally by proportional navigation in pitch of the missile to the target. (Author)

Descriptors :   *Patent applications, *Guidance, *Guided missiles, Antiarmor ammunition, Surface launched, Air launched, Proportional navigation, Yaw, Homing devices, Programmers, Pitch(Motion), Closed loop systems, Control systems, Gimbals, Guided missile trajectories

Subject Categories : Guided Missiles

Distribution Statement : APPROVED FOR PUBLIC RELEASE