• Title/Summary/Keyword: IMU(Inertial Measurement Unit)

Search Result 218, Processing Time 0.026 seconds

Performance Evaluation of a Compressed-State Constraint Kalman Filter for a Visual/Inertial/GNSS Navigation System

  • Yu Dam Lee;Taek Geun Lee;Hyung Keun Lee
    • Journal of Positioning, Navigation, and Timing
    • /
    • v.12 no.2
    • /
    • pp.129-140
    • /
    • 2023
  • Autonomous driving systems are likely to be operated in various complex environments. However, the well-known integrated Global Navigation Satellite System (GNSS)/Inertial Navigation System (INS), which is currently the major source for absolute position information, still has difficulties in accurate positioning in harsh signal environments such as urban canyons. To overcome these difficulties, integrated Visual/Inertial/GNSS (VIG) navigation systems have been extensively studied in various areas. Recently, a Compressed-State Constraint Kalman Filter (CSCKF)-based VIG navigation system (CSCKF-VIG) using a monocular camera, an Inertial Measurement Unit (IMU), and GNSS receivers has been studied with the aim of providing robust and accurate position information in urban areas. For this new filter-based navigation system, on the basis of time-propagation measurement fusion theory, unnecessary camera states are not required in the system state. This paper presents a performance evaluation of the CSCKF-VIG system compared to other conventional navigation systems. First, the CSCKF-VIG is introduced in detail compared to the well-known Multi-State Constraint Kalman Filter (MSCKF). The CSCKF-VIG system is then evaluated by a field experiment in different GNSS availability situations. The results show that accuracy is improved in the GNSS-degraded environment compared to that of the conventional systems.

Real Time Transporter Locating System for Shipyard through GNSS and IMU Sensor (GNSS와 IMU센서를 활용한 실시간 트랜스포터 위치추적 시스템)

  • Mun, SeungHwan;An, JongWoo;Lee, Jangmyung
    • Journal of the Society of Naval Architects of Korea
    • /
    • v.56 no.5
    • /
    • pp.439-446
    • /
    • 2019
  • A real time transporter locating system for shipyard has been implemented through the GNSS and IMU sensor. There are a lot of block movements by transporters at the shipyard, which need to be controlled and monitored for conforming to the shipbuilding process. For the precise and safe transporter motion at the yard, a locating system has been developed by using the GNSS and IMU sensors for the transporter. There are several obstacles of the GPS signals for locating the transporter at the yard, such as, buildings and metal structures. To overcome the weakness of the GPS signal transmission, the IMU data have been properly integrated together. The performance of the proposed real time block locating system has been verified through the real experiments with transporters carrying blocks at a shipyard.

Unlabeled Wi-Fi RSSI Indoor Positioning by Using IMU

  • Chanyeong, Ju;Jaehyun, Yoo
    • Journal of Positioning, Navigation, and Timing
    • /
    • v.12 no.1
    • /
    • pp.37-42
    • /
    • 2023
  • Wi-Fi Received Signal Strength Indicator (RSSI) is considered one of the most important sensor data types for indoor localization. However, collecting a RSSI fingerprint, which consists of pairs of a RSSI measurement set and a corresponding location, is costly and time-consuming. In this paper, we propose a Wi-Fi RSSI learning technique without true location data to overcome the limitations of static database construction. Instead of the true reference positions, inertial measurement unit (IMU) data are used to generate pseudo locations, which enable a trainer to move during data collection. This improves the efficiency of data collection dramatically. From an experiment it is seen that the proposed algorithm successfully learns the unsupervised Wi-Fi RSSI positioning model, resulting in 2 m accuracy when the cumulative distribution function (CDF) is 0.8.

Enhanced Attitude Determination with IMU using Estimation of Lever Arms (레버암 상태 추정을 이용한 IMU 의 자세 결정 알고리즘)

  • Fang, Tae Hyun;Oh, Jaeyong;Park, Sekil;Park, Byoun-Jae;Cho, Deuk-Jae
    • Journal of Institute of Control, Robotics and Systems
    • /
    • v.19 no.10
    • /
    • pp.941-946
    • /
    • 2013
  • In this paper, an enhanced method for attitude determination is proposed for systems using an IMU (Inertial Measurement Unit). In attitude determination with IMU, it is generally assumed that the IMU can be located in the center of gravity on the vehicle. If the IMU is not located in the center of gravity, the accelerometers of the IMU are disturbed from additive accelerations such as centripetal acceleration and tangential acceleration. Additive accelerations are derived from the lever arm which is the distance between the center of gravity and the position of the IMU. The performance of estimation errors can be maintained in system with a non-zero lever arm, if the lever arm is estimated to remove the additive accelerations from the accelerometer's measurements. In this paper, an estimation using Kalman filter is proposed to include the lever arm in the state variables of the state space equation. For the Kalman filter, the process model and the measurement model for attitude determination are made up by using quaternion. In order to evaluate the proposed algorithm, both of the simulations and the experiments are performed for the simplified scenario of motion.

Improvement of the Double Fault Detection Performance of Extended Parity Space Approach (확장 패리티 공간 기법의 이중고장 검출성능 향상 연구)

  • Lee, Won-Hee;Park, Chan-Gook;Lee, Dal-Ho;Kim, Kwang-Hoon
    • Journal of Institute of Control, Robotics and Systems
    • /
    • v.15 no.10
    • /
    • pp.1002-1008
    • /
    • 2009
  • We consider a double faults detection and isolation problem using modified extended parity space approach for inertial measurement unit which use redundant inertial sensors. A redundant IMU which has a hardware redundant is composed of the cone shape because it is good for fault detection and isolation. We analyze the type of double faults and the reason why fault isolation performance is low. We propose modified extended parity space approach method using EPSA and the difference of sensor data.

Fall Risk Assessments Based on Postural and Dynamic Stability Using Inertial Measurement Unit

  • Liu, Jian;Zhang, Xiaoyue;Lockhart, Thurmon E.
    • Safety and Health at Work
    • /
    • v.3 no.3
    • /
    • pp.192-198
    • /
    • 2012
  • Objectives: Slip and fall accidents in the workplace are one of the top causes of work related fatalities and injuries. Previous studies have indicated that fall risk was related to postural and dynamic stability. However, the usage of this theoretical relationship was limited by laboratory based measuring instruments. The current study proposed a new method for stability assessment by use of inertial measurement units (IMUs). Methods: Accelerations at different body parts were recorded by the IMUs. Postural and local dynamic stability was assessed from these measures and compared with that computed from the traditional method. Results: The results demonstrated: 1) significant differences between fall prone and healthy groups in IMU assessed dynamic stability; and 2) better power of discrimination with multi stability index assessed by IMUs. Conclusion: The findings can be utilized in the design of a portable screening or monitoring tool for fall risk assessment in various industrial settings.

An Attitude Determination GPS and INS Integration Scheme: Design and Flight Experiment (자세측정용 GPS/INS 통합시스템 구성 및 비행 시험)

  • Kim, Jeong Won;Hwang, Dong-Hwan;Lee, Sang Jeong;Park, Chansik;Oh, Sang Heon;Kim, Se Hwan;Ahn, Lee-Ki;Lee, Jang-Ho
    • Journal of Advanced Navigation Technology
    • /
    • v.8 no.2
    • /
    • pp.112-119
    • /
    • 2004
  • This paper proposes an attitude determination GPS/INS integrated system scheme for a UAV and presents experimental flight test results. The proposed system is designed as a part of an autopilot system and comprises a GPS attitude determination receiver, an off-the-shelf inertial measurement unit (IMU), and a navigation computer unit (NCU). UAV requires accurate attitude information for stable automatic flight control. The proposed system can provide accurate attitude information for the flight control computer (FCC) so that stable automatic flight control can be achieved. In order to verify the performance of the proposed scheme, an integrated navigation system has been developed. In order to evaluate the developed navigation system, the flight test has been performed. In the flight test, the developed system was shown to provide the position, the velocity and the attitude satisfactorily enough for stable flight control. The accuracy of the attitude information of the developed system was confirmed by comparing attitude of vertical gyro.

  • PDF

Effects of Covariance Modeling on Estimation Accuracy in an IMU-based Attitude Estimation Kalman Filter (IMU 기반 자세 추정 칼만필터에서 공분산 모델링이 추정 정확도에 미치는 영향)

  • Choi, Ji Seok;Lee, Jung Keun
    • Journal of Sensor Science and Technology
    • /
    • v.29 no.6
    • /
    • pp.440-446
    • /
    • 2020
  • A well-known difficulty in attitude estimation based on inertial measurement unit (IMU) signals is the occurrence of external acceleration under dynamic motion conditions, as the acceleration significantly degrades the estimation accuracy. Lee et al. (2012) designed a Kalman filter (KF) that could effectively deal with the acceleration issue. Ahmed and Tahir (2017) modified this method by adjusting the acceleration-related covariance matrix because they considered covariance modeling as a pivotal factor in the estimation accuracy. This study investigates the effects of covariance modeling on estimation accuracy in an IMU-based attitude estimation KF. The method proposed by Ahmed and Tahir can be divided into two: one uses the covariance including only diagonal components and the other uses the covariance including both diagonal and off-diagonal components. This paper compares these three methods with respect to the motion condition and the window size, which is required for the methods by Ahmed and Tahir. Experimental results showed that the method proposed by Lee et al. performed the best among the three methods under relatively slow motion conditions, whereas the modified method using the diagonal covariance with a high window size performed the best under relatively fast motion conditions.

A Study on the Algorithms of Terrestrial Photogrammetry using Vehicle (차량을 이용한 지상사진측량의 알고리즘에 관한 연구)

  • 정동훈;엄우학;김병국
    • Proceedings of the Korean Society of Surveying, Geodesy, Photogrammetry, and Cartography Conference
    • /
    • 2003.04a
    • /
    • pp.145-150
    • /
    • 2003
  • Mobile mapping system is a surveying system that use vehicle carrying various sensors as CCD camera, GPS and IMU(Inertial measurement Unit). This system capturing images of forward direction continuously while running road. Use these images, then acquire road and road facilities information as facilities position, size or maintenance condition. In this study, we organized data and each data processing steps that are needed for 3 dimensional positioning. And develop digital photogrammetry S/W easy to use and accurate for mobile mapping system.

  • PDF

Test-retest Reliability and Intratest Repeatability of Measuring Cervical Range of Motion Using Inertial Measurement Unit (관성측정장치를 이용한 경추관절 가동범위 측정의 검사 내 반복성 및 검사-재검사 신뢰도 연구)

  • Kim, Hyun Ho;Kim, Kyung Wook;Park, Ji Min;Kim, Eun Seok;Lee, Min Jun;Kang, Jung Won;Lee, Sang Hoon;Park, Young Bae
    • Journal of Acupuncture Research
    • /
    • v.30 no.4
    • /
    • pp.25-33
    • /
    • 2013
  • Objectives : To assess the test-retest reliability and the intratest repeatability in measuring the cervical range of motion of healthy subjects with wireless microelectromechanical system inertial measurement unit(MEMS-IMU) system and to discuss the feasibility of this system in the clinical setting to evaluate the cervical spine musculoskeletal. Methods : 12 healthy people who were evaluated as no- or mild-disability with neck disability index were participated. Their cervical motion were measured with IMU twice in consecutive two days for the test-retest reliability study. Intratest repeatability was calculated in the two tests separately. The calculated intraclass correlation coefficients(ICC) were discussed and compared with the those of the previous studies. Results : Cervical range of motion data were acquired and statistically processed: left rotation($61.64^{\circ}$), right rotation($65.12^{\circ}$), extension($61.98^{\circ}$), flexion($52.81^{\circ}$), left bending($39.31^{\circ}$), right bending($41.08^{\circ}$). ICCs were 0.77~0.98(intratest repeatability) and 0.74~0.93 (test-retest reliability) in the primary motion. In the coupling motion, intratest repeatability ICCs were 0.93~ 0.99(transverse primary plane), 0.88~0.97(saggital primay plane), and 0.77~0.93(coronal primary plane). Test-retest reliability of coupling motion were 0.90~0.97(transverse primary plane), 0.00~0.72(saggital primary plane), and 0.04~0.76(coronal primary plane). Conclusions : Several types of range-of-motion devices are now on use in many fields including medicine, but the practicality of the devices in clinical use is questionable for the convenient and economical aspects. In this study, we presented the reliability of cervical range of motion test with the developed wireless MEMS-IMU system and discussed its potential utility in clinical use.