| A Test Technique for Performance Evaluation of a Filter and Control Loop on the Missile Vibration using Floating System |
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KyungHwan Kim, BumSoo Park, Hyun Lee, SangJae Kim, JaeWook Chung |
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The 1st Research and Development Institute, Agency for Defense Development |
| 부유시스템을 이용한 유도탄 조종루프 진동저감 성능확인 시험기법 |
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김경환, 박범수, 이현, 김상재, 정재욱 |
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국방과학연구소 제1기술연구본부 |
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| Abstract |
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The acceleration and the angular velocity that include natural frequencies of a missile detected by Inertial Measurement Unit(IMU) are transmitted to the control loop of a missile. The control loop command that is calculated using above signals can cause the resonance of the missile while it flies. Hence it is common to adapt the filter and the control loop for attenuating or eliminating the undesired signals such as natural frequencies. This paper introduces the new test technique using a floating system for performance evaluation of the designed filter and the control loop prior to a flight test. The proposed scheme can check out the degradation property of vibration in the filter and the control loop, while the conventional hardware-in-the-loop simulation(HILS) scheme cannot. |
| Key Words:
Control Loop, Inertial Measurement Unit, Floating System, Filter, Hardware-in-the-loop Simulation |
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