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Celia Bartel

Researcher at Cranfield University

Publications -  10
Citations -  175

Celia Bartel is an academic researcher from Cranfield University. The author has contributed to research in topics: Navigation system & Inertial measurement unit. The author has an hindex of 8, co-authored 10 publications receiving 170 citations.

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A Low-cost Vision Based Navigation System for Small Size Unmanned Aerial Vehicle Applications

TL;DR: A low cost navigation system based on Vision Based Navigation and other avionics sensors is presented, which is designed for small size Unmanned Aerial Vehicle (UAV) applications and shows that the integrated system can reach position, velocity and attitude accuracies compatible with CAT-II precision approach requirements.

Carrier-phase GNSS attitude determination and control system for unmanned aerial vehicle applications

TL;DR: Modelling and simulation activities focussed on the AEROSONDE UAV platform and considered the possible augmentation provided by interferometric GNSS techniques to a low-cost and low-weight/volume integrated navigation system recently developed at Cranfield University.
Journal Article

Navigation and Guidance System Architectures for Small Unmanned Aircraft Applications

TL;DR: A compact, light and relatively inexpensive system capable of providing the required navigation performance in all phases of flight of small UA, with a special focus on precision approach and landing, where Vision Based Navigation techniques can be fully exploited in a multisensor integrated architecture.
Journal ArticleDOI

Low-cost navigation and guidance systems for unmanned aerial vehicles - part 1: Vision-based and integrated sensors

TL;DR: A compact, light and relatively inexpensive system capable of providing the Required Navigation Performance (RNP) in all phases of flight of a small UAV, with a special focus on precision approach and landing, where Vision Based Navigation (VBN) techniques can be fully exploited in a multisensor integrated architecture.
Journal ArticleDOI

Low-cost navigation and guidance systems for unmanned aerial vehicles - part 2: Attitude determination and control

TL;DR: In this paper, a carrier-phase Global Navigation Satellite Systems (GNSS) for attitude determination and control of small to medium size UAVs is presented, where recursive optimal estimation algorithms are developed for combining multiple attitude measurements obtained from different observation points (i.e., antenna locations).