한국군사과학기술학회지 (Journal of the Korea Institute of Military Science and Technology)

  • 제21권3호
  • /
  • Pages.349-360
  • /
  • 2018
  • /
  • 1598-9127(pISSN)
  • /
  • 2636-0640(eISSN)
한국군사과학기술학회 (The Korea Institute of Military Science and Technology)
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관성항법장치가 포함된 비행체의 HWIL 시뮬레이션 시스템 개발 연구

A Study on the HWIL Simulation System of the Flight Object including Inertial Navigation System

  • 이아영 (국방과학연구소 제1기술연구본부)
  • Lee, Ayeong (The 1st Research and Development Institute, Agency for Defense Development)
  • 투고 : 2017.11.27
  • 심사 : 2018.05.11
  • 발행 : 2018.06.05
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초록

This paper proposes various methods for constructing a HWIL simulation system including Inertial Navigation System(INS) and Guidance Control Unit(GCU) under the assumption that the INS identifies the initial attitude of an aviation body through its own alignment and that it is a package consisting of an inertial sensor and a navigation computation module. This paper also presents a real-time computing technology and a way to calculate the command of the Flight Motion System(FMS) analogous to the acutal flight environment. The proposed HWIL simulation system is constructed by applying the above-mentioned methods and the results of running a series of simulations confirm high effectiveness and usefulness of the system. Finally, minor error factors that could be acquired only in HWIL simulation Environment are analyzed.

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참고문헌

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