• Title/Summary/Keyword: 관성측정기

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Life Test Design and Evaluation of Inertial Measurement Unit for Guided Weapons (유도무기용 관성측정기 수명 시험 설계 및 평가)

  • Jo, Kyoung Hwan;Moon, Sang Chan;Yun, Suk Chang;Kwon, Seung Bok;Kim, Do Hyung;Yang, Il Young
    • Journal of Aerospace System Engineering
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    • v.16 no.5
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    • pp.94-101
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    • 2022
  • In this paper, we have obtained the acceleration coefficient of the IMU (Inertial Measurement Unit) to prove reliability by analyzing the characteristic of the MEMS IMU installed in guided weapon systems for overseas export and the operating environment of the guided weapon system. Additionally, based on designed life testing, we performed life tests on three the IMUs and demonstrated a target lifetime of 12 years.

Performance verification methods of an inertial measurement unit in flight environment using the real time dual-navigation (실시간 다중항법을 이용한 관성측정기의 비행환경 성능 검증 기법)

  • Park, ByungSu;Lee, SangWoo;Jeong, Sang Mun;Han, KyungJun;Yu, Myeong-Jong
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.45 no.1
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    • pp.36-45
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    • 2017
  • Abstract It is necessary to verify the properties of an inertial measurement unit in the flight environment before applying to military applications. In this paper, we presented a new approach to verify an inertial measurement unit(IMU) in regard to the performance and the robustness in flight environments for the high-dynamics vehicle systems. We proposed two methods for verification of an IMU. We confirmed normal operation of an IMU and properties in flight environment by using direct comparison method. And we proposed real time multi-navigation system to complement the first method. The proposed method made it possible to compare navigation result at the same time. Therefore, it is easy to analyze the performance of an inertial navigation system and robustness during the vehicle flight. To verify the proposed method, we carried out a flight test as well as an experimental test of flight vibration on the ground. As a result of the experiment, we confirmed flight environment properties of an IMU. Therefore, we shows that the proposed method can serve the reliability improvement of IMU.

LOS Determination Using INS for an Aircraft Mounted Satellite Tracking Antenna (관성측정기를 이용한 항공기용 위성추적 안테나의 지향각 결정)

  • Jung, Ha-Hyoung;Kim, Chung-Il;Lyou, Joon
    • Journal of the Institute of Electronics Engineers of Korea SC
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    • v.49 no.3
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    • pp.12-18
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    • 2012
  • This paper presents a computation method of LOS(Line Of Sight) angle using IMU(Inertial Measurement Unit) for an antenna on aerial vehicle to point to a stationary satellite. In the overall system, the antenna is located at the front of the vehicle, and an IMU is introduced to account for body flexure dynamic. And using the differences between the position and velocity of the IMU based navigation and those of GPS/INS at the vehicle center. Kalman filter is designed to suppress Strapdown INS drift errors.

A Study on the Multipurpose Golf Putting Range Finder using IR Razer Sensor and Inertial Sensor (IR 레이저 센서 및 관성 센서를 이용한 다목적 골프 퍼팅 거리 측정기에 대한 연구)

  • Min-Seoung Shin;Dae-Woong Kang;Ki-Deok Kim;Ji-Hwan Kim;Chul-Sun Lee;Yun-Seok Ko
    • The Journal of the Korea institute of electronic communication sciences
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    • v.18 no.4
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    • pp.669-676
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    • 2023
  • In this paper, a multi-purpose golf putting range finder based on an IR razer sensor and an inertial sensor was designed and made. It was designed to measure distance and slope within a 50m outdoor measurement range for the main purpose of golf putting distance measurement, and at the same time, it is designed to measure temperature information that affects putting. In addition, the distance meter supports house maintenance work by providing length and horizontality measurement values within the indoor 80m measurement range, and provides safety from indoor or vehicle fires by providing indoor temperature measurement values to mobile phones through linkage with the web server. In order to evaluate the accuracy of the proposed method and its interworking performance with a smartphone, a prototype was produced and a web server was built, and the usefulness was confirmed by showing an acceptable error rate within 5% in repeated experiments.

The Extraction Method for the G-Sensitivity Scale-Factor Error of a MEMS Vibratory Gyroscope Using the Inertial Sensor Model (관성센서 오차 모델을 이용한 진동형 MEMS 자이로스코프 G-민감도 환산계수 오차 추출 기법)

  • Park, ByungSu;Han, KyungJun;Lee, SangWoo;Yu, MyeongJong
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.47 no.6
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    • pp.438-445
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    • 2019
  • In this paper, we present a new approach to extract the g-sensitivity scale-factor error for a MEMS gyroscope. MEMS gyroscopes, based on the use of both angular momentum and the Coriolis effect, have a g-sensitivity error due to mass unbalance. Generally, the g-sensitivity error is not considered in general use of gyroscopes, but it deserves our attention if we are to develop for tactical class performance and reliability. The g-sensitivity error during vehicle flight increases navigation error; so it must be analyzed and compensated for the use of MEMS IMU for high dynamics vehicle systems. Therefore, we analyzed how to extract the g-sensitivity scale-factor error from the inertial sensor error model. Furthermore we propose a new method to extract the g-sensitivity error using flight motion simulator. We verified our proposed method with experimental results.

Calibration Technique of Strapdown Iinertial Measurement Unit Using Kalman Filter (칼만필터를 이용한 스트랩다운 관성측정기의 교정기법)

  • Kim, Cheon-joong;Song, Ki-Won;Lyou, Joon
    • 제어로봇시스템학회:학술대회논문집
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    • 1993.10a
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    • pp.304-307
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    • 1993
  • In this paper, we formulate Kalman filter for calibration of strapdown inertial measurment unit(SDIMU) on navigation system level and analyize its performance by covariance simulation method. It has been shown that the calibration method suggested in this paper is not largely influenced by accuracy of a mounting axis alignment required in calibration of SDIMU on IMU level.

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Analysis of Navigation Error According to Rotational Motions of Rotational Inertial Navigation for Designing Optimal Rotation Sequence (최적 회전 절차 설계를 위한 회전형 관성항법장치의 회전 동작별 항법 오차 분석)

  • Jae-Hyuck Cha;Chan-Gook Park;Seong-Yun Cho;Min-Su Jo;Chan-Ju Park
    • The Journal of the Korea institute of electronic communication sciences
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    • v.19 no.2
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    • pp.445-452
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    • 2024
  • This paper analyzes the navigation error for each rotational motion in order to design an optimal rotation sequence, which is a key technology in the rotational inertial navigation. Rotational inertial navigation system is designed to cancel out navigation errors caused by inertial sensor errors by periodically rotating the inertial measurement unit. A properly sequenced rotational motion cancels out the maximum amount of navigation error and is known as an optimal rotation sequence. To design such an optimal turning procedure, this paper identifies the feasible rotational motions that can be implemented in a rotational inertial navigation system and analyzes the navigation error introduced by each rotational motion. In addition, by analyzing the characteristics of the navigation error generated during a rotation sequence in combination, this paper presents the conditions for designing an optimal rotation sequence.

Classification of the Korean Road Roughness (국내 도로면 거칠기 특성 분류 기준에 관한 연구)

  • Choi, Gyoo-Jae;Heo, Seung-Jin
    • Transactions of the Korean Society of Automotive Engineers
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    • v.14 no.5
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    • pp.115-120
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    • 2006
  • A Korean Road Roughness Classification(KRC) method is proposed. Using a dynamic road profiling device equipped with the Accelerometer Established Inertial Profiling Reference(AEIPR) method, road profile measurement is performed on various types of public paved roads in Korea. The road profiling data are processed to classify the characteristics of Korean road roughness. The resultant Korean road roughness classification(KRC) is shown different characteristics compared to the road classification proposed by ISO, MIRA, and Wong. The proposed KRC is composed of 8 classes(A-H, very good-poor) based on the power spectral density and is in good agreements with the characteristics of Korean paved road roughness and can be used well in vehicle ride comfort simulation using domestic road profile.

An Implementation of Mobile Respiration Detection Diagnostic System Using Ultrasound Sensing Method (초음파 센싱 방식의 이동형 호흡 측정 진단 시스템의 구현)

  • 김동학;김영길;정승호
    • Proceedings of the Korean Institute of Information and Commucation Sciences Conference
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    • 2003.05a
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    • pp.514-517
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    • 2003
  • Oxygen supply is one of the most basic things in human body. Breathing is controlled by the lungs' stationary function and the respiratory center which is in the mesulla oblongata. Nothing but, the external breathing that air movement between the lungs and atmosphere and the internal breathing that cellular air movement between the hemoglobin and a single cell. The adult's number of times of the respirations is about 15∼20 per 1 minute, but it depends ages, exercise, temperature, disease, etc. The important thing in detecting the respiration is that doing it in object person's resting time. Detecting the respiration have to be done without attracting any attention of object person. In present using method is detecting the pulse with catching an object person's wrist and observing the object person's movement. In this paper, we propose the mobile respiration detection diagnostic system using ultrasound sensing method that does not be influenced by the inertia error and the pressure error.

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Design and Implementation of Mobile ]Respiration Detection Diagnostic System using Ultrasound Sensing Method fficient Multicasting Environment (초음파 센싱 방식을 이용한 이동형 호흡량 측정 진단기의 설계 및 구현)

  • 김동학;김영길
    • Journal of the Korea Institute of Information and Communication Engineering
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    • v.8 no.2
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    • pp.509-515
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    • 2004
  • Pulmonary function tests are widely used to diagnose and determine patients' therapy in clinic. And it was also applied in the research of the physiology and dynamics for lung disease. Among the pulmonary function tests, spirometry is the most easy and economic test. Spirometers are medical instruments that measure the instantaneous rate of volume flow of respired Bas. The mechanical spirometer was mostly used in the past. Up to the present, the most popular method of spirometer is the differential pressure technique with which change in the volume of flow are transferred to change in pressure. This kind of instrument suffers from several limitations, pressure drop, difficulty in maintenance and short period of calibration. Therefore, this study has begun to implement ultrasound spirometer, which is free of pressure loss and has wide range, focusing on the flow measurement technique and diagnostic algorithm.