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HELICOPTER INTEGRATED FIRE AND FLIGHT CONTROL HAVING CONSTRAINT LIMITING CONTROL
HELICOPTER INTEGRATED FIRE AND FLIGHT CONTROL HAVING CONSTRAINT LIMITING CONTROL
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机译:具有约束限制控制的直升机综合火力和飞行控制
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摘要
During operation of an integrated fire and flight control (IFFC) system in a coupled aiming mode, the occurrence of a weapon (172), weapon mount (145) or sensor (146) reaching a constraint limit (210) indices a fade-in of a constraint limiting axis command signal (140) for a respective attitude axis as the aircraft attitude reference, replacing the flight control system attitude feedback error signal (111) for the respective attitude axis. The constraint limiting axis command signals provide the aircraft attitude reference only while the pilot manually depresses and holds an enable switch (920). The pilot command stick input (90) remains the primary input to the IFFC system to thereby provide override capability for pilot command maneuvers.
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