Describes briefly two existing anti-radiation missile (ARM) seeker follow-up systems, viz. the hydraulic pressure servo ARM seeker follow-up system and eiectromotion ARM seeker follow-up system. On the basis of retaining their superiority, a new strapdown ARM seeker follow-up system with better per?formances was suggested. In this system the inertial measurement unit is fixed on the vehicle directly. It adopts the classical proportional integral differential control, witn its servomechanism adopting DC moment motor driven by pulse width modulation working on proportion guidance. The paper analyzed the perfor?mance and characteristics of the ARM seeker follow-up system in detail. Theoretical analysis and simulation show that the ARM seeker follow-up system inherits the excellence of the above two ARM seeker follow-up systems that the structure of the system is simple, and that the effect of the missile attitude movement to steady-state response of the ARM seeker follow-up system is eliminated with integral control. Simulation results also show that the designed system has good tracking performance.
Yang Yanjuan ,Jin Zhihua, Tian Weifeng.
Design of Anti-Radiation Missile Seeker Follow-Up System Driven by Pulse-Width Modulation. Acta Armamentarii. 2004, 25(2): 214-217 https://doi.org/10.3969/j.issn.1000-1093.2004.02.022
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