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http://dx.doi.org/10.9766/KIMST.2019.22.4.536

A Study On Missile Flight Simulation Method Using the Built-in Memory of Aviation Control Unit  

Kim, Tae-Hoon (The 1st Research and Development Institute, Agency for Defense Development)
Lee, Sang-Hoon (The 1st Research and Development Institute, Agency for Defense Development)
Gong, Min-Sik (The 1st Research and Development Institute, Agency for Defense Development)
Publication Information
Journal of the Korea Institute of Military Science and Technology / v.22, no.4, 2019 , pp. 536-544 More about this Journal
Abstract
During the assembly and function inspection of missile system, flight simulation process is required. In the conventional flight simulation check of missiles, an inertial navigation system simulator was used to transmit the navigation output data acquired in HILS. There are several disadvantages in terms of check configuration complexity and data synchronization when using the simulator. So we proposed a new flight simulation method that utilizes the nonvolatile built-in memory of the aviation control unit. The data processing procedure and operation procedure of the proposed method for type I and type II missiles are presented. And we analyzed the causes of the difference between proposed method result and the HILS result for type II missile. By comparing the results obtained by the experiments using the proposed method with the results of HILS, the validity of proposed method was confirmed.
Keywords
Missile Flight Simulation; Navigation Output Data; Nonvolatile Built-in Memory;
Citations & Related Records
Times Cited By KSCI : 1  (Citation Analysis)
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