Aboelmagd Noureldin

Prof. Aboelmagd Noureldin

Professor, Department of Electrical and Computer Engineering, Royal Miliatry College of Canada
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orcid

Research Focus & Metrics

Academic Career Length

21Years (2006-Present)

(Calculated once Scilit publication data is synced: current year − year of first publication + 1)

Representative Publications

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1 January 2013
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Book
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Aboelmagd NoureldinAboelmagd Noureldin
Aboelmagd Noureldin
TKTashfeen B. Karamat
Tashfeen B. Karamat
JGJacques Georgy
Jacques Georgy

23 May 2008 in IEEE Transactions on Vehicular Technology
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Journal Article
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Aboelmagd NoureldinAboelmagd Noureldin
Aboelmagd Noureldin
TKTashfeen B. Karamat
Tashfeen B. Karamat
EBEberts
Eberts
Ahmed ElshafieAhmed Elshafie
Ahmed Elshafie
MEMark D. Eberts
Mark D. Eberts
The relatively high cost of inertial navigation systems (INSs) has been preventing their integration with global positioning systems (GPSs) for land-vehicle applications. Inertial sensors based on microelectromechanical system (MEMS) technology have recently become commercially available at lower costs. These relatively lower cost inertial sensors have the potential to allow the development of an affordable GPS-aided INS (INS/GPS) vehicular navigation system. While MEMS-based INS is inherently immune to signal jamming, spoofing, and blockage vulnerabilities (as opposed to GPS), the performance of MEMS-based gyroscopes and accelerometers is significantly affected by complex error characteristics that are stochastic in nature. To improve the overall performance of MEMS-based INS/GPS, this paper proposes the following two-tier approach at different levels: (1) improving the stochastic modeling of MEMS-based inertial sensor errors using autoregressive processes at the raw measurement level and (2) enhancing the positioning accuracy during GPS outages by nonlinear modeling of INS position errors at the information fusion level using neuro-fuzzy (NF) modules, which are augmented in the Kalman filtering INS/GPS integration. Experimental road tests involving a MEMS-based INS were performed, which validated the efficacy of the proposed methods on several trajectories.

1 January 2011 in Information Fusion
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Journal Article
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Aboelmagd NoureldinAboelmagd Noureldin
Aboelmagd Noureldin
Ahmed ElshafieAhmed Elshafie
Ahmed Elshafie
MBMohamed Bayoumi
Mohamed Bayoumi

29 June 2006 in Water Resources Management
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Ahmed ElshafieAhmed Elshafie
Ahmed Elshafie
Mahmoud Reda TahaMahmoud Reda Taha
Mahmoud Reda Taha
Aboelmagd NoureldinAboelmagd Noureldin
Aboelmagd Noureldin

15 September 2015 in Sensors
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YGYanbin Gao
Yanbin Gao
SLShifei Liu
Shifei Liu
MAMohamed Atia
Mohamed Atia
Aboelmagd NoureldinAboelmagd Noureldin
Aboelmagd Noureldin
This paper takes advantage of the complementary characteristics of Global Positioning System (GPS) and Light Detection and Ranging (LiDAR) to provide periodic corrections to Inertial Navigation System (INS) alternatively in different environmental conditions. In open sky, where GPS signals are available and LiDAR measurements are sparse, GPS is integrated with INS. Meanwhile, in confined outdoor environments and indoors, where GPS is unreliable or unavailable and LiDAR measurements are rich, LiDAR replaces GPS to integrate with INS. This paper also proposes an innovative hybrid scan matching algorithm that combines the feature-based scan matching method and Iterative Closest Point (ICP) based scan matching method. The algorithm can work and transit between two modes depending on the number of matched line features over two scans, thus achieving efficiency and robustness concurrently. Two integration schemes of INS and LiDAR with hybrid scan matching algorithm are implemented and compared. Real experiments are performed on an Unmanned Ground Vehicle (UGV) for both outdoor and indoor environments. Experimental results show that the multi-sensor integrated system can remain sub-meter navigation accuracy during the whole trajectory.

1 July 2010 in IEEE Transactions on Intelligent Transportation Systems
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Journal Article
Closed access
JGJacques Georgy
Jacques Georgy
Aboelmagd NoureldinAboelmagd Noureldin
Aboelmagd Noureldin
MKMichael J. Korenberg
Michael J. Korenberg
MBMohamed M. Bayoumi
Mohamed M. Bayoumi
To have a continuous navigation solution that does not suffer from interruption, GPS is integrated with relative positioning techniques such as odometry and inertial navigation. Targeting a low-cost navigation solution for land vehicles, this paper uses a reduced multisensor system consisting of one microelectromechanical-system (MEMS)-based single-axis gyroscope used together with the vehicle's odometer, and the whole system is integrated with GPS. This system provides a 2-D navigation solution, which is adequate for land vehicles. The traditional technique for this multisensor integration problem is Kalman filtering (KF). Due to the inherent errors of MEMS inertial sensors and their stochastic nature, which is difficult to model, the KF with its linearized models has limited capabilities in providing accurate positioning. Particle filtering (PF) has recently been suggested as a nonlinear filtering technique to accommodate arbitrary inertial sensor characteristics, motion dynamics, and noise distributions. An enhanced version of PF is utilized in this paper and is called the Mixture PF. Since PF can accommodate nonlinear models, this paper uses total-state nonlinear system and measurement models. In addition, sophisticated models are used to model the stochastic drift of the MEMS-based gyroscope. A nonlinear system identification technique based on parallel cascade identification (PCI) is used to model this stochastic gyroscope drift. In this paper, the performance of the PCI model is compared with that of higher order autoregressive (AR) stochastic models. Such higher order models are difficult to use with KF since the size of the dynamic matrix and the error-covariance matrix becomes very large and complicates the KF operation. The performance of the proposed 2-D navigation solution using Mixture PF with both PCI and higher order AR models is examined by road-test trajectories in a land vehicle. The two proposed combinations are compared with four other 2-D solutions: a Mixture PF with the Gauss-Markov (GM) model for the gyro drift, a Mixture PF with only white Gaussian noise (WGN) for stochastic gyro errors, and two different KF solutions with GM model for the gyro drift. The experimental results show that the two proposed solutions outperform all the compared counterparts.