Publication:
Personal inertial navigation system assisted by mems ground reaction sensor array and interface ASIC for GPS-denied environment

dc.contributor.authorGuo, Q.
dc.contributor.authorDeng, W. H.
dc.contributor.authorBebek, Özkan
dc.contributor.authorCavusoglu, M. C.
dc.contributor.authorMastrangelo, C. H.
dc.contributor.authorYoung, D. J.
dc.contributor.departmentMechanical Engineering
dc.contributor.ozuauthorBEBEK, Özkan
dc.date.accessioned2019-02-12T06:06:13Z
dc.date.available2019-02-12T06:06:13Z
dc.date.issued2018-11
dc.description.abstractA personal inertial navigation system (PINS) assisted by a microelectromechanical systems (MEMS)-based 13 × 26 ground reaction sensor array (GRSA) and a low-power interface application-specified integrated circuit (ASIC) has been designed and demonstrated for GPS-denied environment. The GRSA operating in a contact mode achieves a sensitivity of approximately 3.7 fF/kPa at each sensor node. An electronic interface system, consisting of a capacitance-to-voltage (C/V) converter followed by a correlated double sampling stage, is designed to convert the GRSA capacitance change to an analog output voltage. The analog output voltage is then digitized by a 12-bit cyclic analog-to-digital converter (ADC). Switch capacitance compensation technique is employed to ensure the ADC performance. The ASIC is fabricated in 0.35-μm CMOS process and dissipates a power of 3 mW. The prototype system incorporates a GRSA, an ASIC, and a commercial nine degreeof-freedom (DOF) inertial measurement unit (IMU) in the heel region of a boot. The GRSA can determine an accurate foot-onground timing based on the pressure profiles detected during walking, thus enabling an accurate position calculation and a precise zero velocity update. Furthermore, a system calibration procedure measures the IMU inherent directional drift and scaling factor errors, and compensates them for the navigation data to achieve a superior performance. The prototype system demonstrates a position accuracy of approximately 5.5 m over a navigation distance of 3100 m. The prototype system also achieves a consistent performance over different field tests with various distances and random paths. System characterization results further indicate a tradeoff between sensor array size and system resolution for a given navigation performance requirement, thus providing a design guideline for future system optimization.en_US
dc.description.sponsorshipUtah Science Technology and Research ; University of Utah ; University of London
dc.identifier.doi10.1109/JSSC.2018.2868263en_US
dc.identifier.endpage3049en_US
dc.identifier.issn0018-9200en_US
dc.identifier.issue11en_US
dc.identifier.scopus2-s2.0-85054493368
dc.identifier.startpage3039en_US
dc.identifier.urihttp://hdl.handle.net/10679/6169
dc.identifier.urihttps://doi.org/10.1109/JSSC.2018.2868263
dc.identifier.volume53en_US
dc.identifier.wos000449108400004
dc.language.isoengen_US
dc.peerreviewedyesen_US
dc.publicationstatusPublisheden_US
dc.publisherIEEEen_US
dc.relation.ispartofIEEE Journal of Solid-State Circuits
dc.relation.publicationcategoryInternational Refereed Journal
dc.rightsrestrictedAccess
dc.subject.keywordsCapacitance-to-voltage (C/V) converteren_US
dc.subject.keywordsCapacitive sensoren_US
dc.subject.keywordsCyclic analog-to-digital converteren_US
dc.subject.keywordsGPS-denied navigationen_US
dc.subject.keywordsGround reaction sensor array (GRSA)en_US
dc.subject.keywordsInertial measurement unit (IMU)en_US
dc.subject.keywordsPersonal inertial navigation system (PINS)en_US
dc.subject.keywordsPressure sensor arrayen_US
dc.subject.keywordsSwitch capacitance compensationen_US
dc.subject.keywordsTactile sensor arrayen_US
dc.titlePersonal inertial navigation system assisted by mems ground reaction sensor array and interface ASIC for GPS-denied environmenten_US
dc.typearticleen_US
dspace.entity.typePublication
relation.isOrgUnitOfPublicationdaa77406-1417-4308-b110-2625bf3b3dd7
relation.isOrgUnitOfPublication.latestForDiscoverydaa77406-1417-4308-b110-2625bf3b3dd7

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