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류무용,Ryu, Moo-Yong 한국군사과학기술학회 2008 한국군사과학기술학회지 Vol.11 No.2
A distributed missile system is composed of command control center, radar and launcher which exchange information each other to use wire or wireless network. The distributed missile system is required mobility for operational convenience and survivability. Also missile system requests land navigation system to provide relatively accurate attitude. For reason of these requirements, each subsystem needs land navigation which provides information of position and attitude. This paper represents operational concept for land navigation to consider operational environment and concrete operational procedure to apply the operational concept. In state that there is no operation for land navigation of distributed missile system internally so for, this paper could be helped to establish operational concept and procedure of this kind of system.
A Study for Measuring Assembly Misalignment of High Maneuver Precision Guidance Missile
최승혁(Seung Hyuk Choi),이광원(Kwang Won Lee),류무용(Moo Yong Ryu),안성용(Sung Yong An),이동주(Dong Ju Lee) Korean Society for Precision Engineering 2019 한국정밀공학회지 Vol.36 No.10
The assembly misalignment of a high maneuver precision guidance missile such as anti-air interceptor could have poor influence on the performance of the system and lead to fatal mission failure. Thus, several methods to minimize the assembly misalignment of missiles have been suggested, including assembly guiding tools and measuring devices. However, previously suggested solutions have disadvantages in versatility and cost. In this study, the low cost and universally applicable solution based on inclinometers for measuring assembly misalignment of a missile is introduced. The comparison between measurement data of the suggested system and a three-dimensional laser tracker for a missile assembly misalignment was conducted. The results show the suggested system can quantify a missile assembly misalignment with comparable precision and accuracy.