• 제어로봇시스템학회:학술대회논문집
• /
• 제어로봇시스템학회 1988년도 한국자동제어학술회의논문집(국내학술편); 한국전력공사연수원, 서울; 21-22 Oct. 1988
• /
• pp.649-653
• /
• 1988

The inertial measurement units in Strapdown System are characterized by the fact that sensors directly mounted to the vehicle frame. So the sensors are subjected to the translatory and rotation dynamics of the vehicle. The sensor outputs involve many error terms. We must compensate the error terms for accuracy improvement. The method which identify the error parameter is studied and suggested.

• 한국정밀공학회:학술대회논문집
• /
• 한국정밀공학회 2008년도 춘계학술대회 논문집
• /
• pp.661-662
• /
• 2008

• 한국통신학회논문지
• /
• 제40권2호
• /
• pp.397-407
• /
• 2015

본 논문에서는 최근 스마트폰이나 웨어러블 디바이스처럼 IoT/M2M 을 위한 여러 종류의 모바일 기기에 사용되는 센서 중에서 각속도를 검출하는데 사용되는 3축 자이로스코프 센서 IC와 가속도를 검출하는데 사용되는 3축 가속도 센서IC를 1 chip으로 하는 6축 관성센서 IC를 설계하였다. 특히 본 논문에는 자이로스코프 센서의 잡음을 분석하고 이를 효과적으로 제거하기 위한 구조를 제안하였다. 자이로스코프 센서는 가속도 센서, 지자기 센서와 더불어 사용자의 동작을 인식하고, 상대적 위치를 추정하기 위한 용도로 사용되는 센서이다. 위치를 추정할 때 사용되는 센서는 아주 작은 잡음이라도 오차로 누적되기 때문에, 정확도를 높이기 위해서 저잡음 IC 설계가 아주 중요한 요소이다. 본 논문에서는 자이로스코프 센서를 모델링하고 MEMS(micro-electro-mechanical system)와 회로에서 발생하는 잡음의 주파수 특성을 분석하여 이를 효과적으로 제거하기 위한 회로 구조를 제안하였으며, 초소형, 저전력 환경에서 사용 가능하면서 잡음 수준이 아주 낮은 3축 자이로스코프 센서와 3축 가속도 센서를 포함하는 6축 1 chip IC를 제작하였다. 제작된 IC는 자이로스코프 센서 잡음의 주요 원인이 되는 quadrature error를 효과적으로 제거하기 위한 회로 구조를 사용하였고, 0.18um CMOS공정을 이용하여 0.01dps/${\sqrt{Hz}}$의 자이로스코프 센서 잡음밀도를 가지는 IC를 제작하였다.

• 제어로봇시스템학회논문지
• /
• 제16권12호
• /
• pp.1167-1175
• /
• 2010

This paper presents the use of the inertial measurement unit information and the infrared sector information for getting the position of an object. Travel distance is usually calculated from the double integration of the accelerometer output with respect to time; however, the accumulated errors due to the drift are inevitable. The orientation change of the accelerometer also causes error because the gravity is added to the measured acceleration. Unless three axis orientations are completely identified, the accelerometer alone does not provide correct acceleration for estimating the travel distance. We propose a way of minimizing the error due to the change of the orientation. In order to reduce the accumulated error, the infrared sector information is fused with the inertial measurement unit information. Infrared sector information has highly deterministic characteristics, different from RFID. By putting several infrared emitters on the ceiling, the floor is divided into many different sectors and each sector is set to have a unique identification. Infrared light based sector information tells the sector the object is in, but the size of the uncertainty is too large if only the sector information is used. This paper presents an algorithm which combines both the inertial measurement unit information and the sector information so that the size of the uncertainty becomes smaller. It also introduces a framework which can be used with other types of the artificial landmarks. The characteristics of the developed infrared light based sector and the proposed algorithm are verified from the experiments.

• 제어로봇시스템학회:학술대회논문집
• /
• 제어로봇시스템학회 1997년도 한국자동제어학술회의논문집; 한국전력공사 서울연수원; 17-18 Oct. 1997
• /
• pp.1679-1683
• /
• 1997

In this paper a linear Kalman filter for calibration of gimballed inertial navigation system(GINS) is designed and its performace is analyzed through the simulation with a real navigation data. Simulation results show that the proposed Kalman filter gives a good performance to calibrate the sensor errors.

• 해양환경안전학회:학술대회논문집
• /
• 해양환경안전학회 2018년도 공동국제학술발표회
• /
• pp.80-80
• /
• 2018

• 센서학회지
• /
• 제23권4호
• /
• pp.251-258
• /
• 2014

While the feasibility of vertical velocity as a threshold parameter for pre-impact fall detection has been verified, effects of sensor attachment locations and methods calculating vertical acceleration and velocity on the detection performance have not been studied yet. Regarding the vertical velocity-based pre-impact fall detection, this paper investigates detection accuracies of eight different cases depending on sensor locations (waist vs. sternum), vertical accelerations (accurate acceleration based on both accelerometer and gyroscope vs. approximated acceleration based on only accelerometer), and vertical velocities (velocity with attenuation vs. velocity difference). Test results show that the selection of waist-attached sensor, accurate acceleration, and velocity with attenuation based on accelerometer and gyroscope signals is the best in overall in terms of sensitivity and specificity of the detection as well as lead time.

• 제어로봇시스템학회논문지
• /
• 제8권8호
• /
• pp.698-705
• /
• 2002

The redundant sensor configuration problem of inertial navigation system(INS) is considered and analyzed the navigation and fault detection performance according to various sensor configurations. We considered various kinds of redundant sensor configurations for symmetric, cone, and orthogonal configurations and compare the navigation and fault detection performance for the configurations. We show that the navigation and fault detection performance is not affected by the coordinate change for a fixed configuration.

• 제어로봇시스템학회논문지
• /
• 제12권10호
• /
• pp.982-988
• /
• 2006

The errors of INS (Inertial Navigation System) are known to grow in time. To compensate the accumulated errors, measurements of external or onboard sensors are extensively utilized to form an integrated navigation system. Recently, INS/GPS integrated navigation systems have become popular since exact position and velocity information can be utilized by low cost GPS receivers. Unfortunately, this configuration cannot be trusted at all times especially when there are intentional or unexpected jammings and interruptions. To aid INS irrespectively of these cases, an INS/Image sensor integrated navigation system configuration is designed only based on the information of image sensor gimble angles. The performance of the INS/Image sensor integrated navigation system is evaluated by Monte Carlo simulation.

• International Journal of Ocean System Engineering
• /
• 제1권3호
• /
• pp.165-170
• /
• 2011

In this paper, for the accurate estimation of the position and orientation of the UUV (unmanned underwater vehicle), an AHRS (Attitude Heading Reference System) was developed using the IMU (inertial measurement unit) sensor which provides information on acceleration and orientation in the object coordinate and the initial alignment algorithm and the E-KF (extended Kalman Filter). The initial position and orientation of the UUV are estimated using the initial alignment algorithm with 3-axis acceleration and geomagnetic information of the IMU sensor. The position and orientation of the UUV are estimated using the AHRS composed of 3-axis acceleration, velocity, and geomagnetic information and the E-KF. For the performance test of the orientation estimation of the AHRS, a testbed using IMU sensor(ADIS16405) and DSP28335 coded with an E-KF algorithm was developed and its performance was verified through tests.