Kevin Worrall
Current Organizations / Institutes
The organizations/institutes from the scholar's latest article
Research Subjects
Kevin Worrall has a total of 28 co-authors. Here are the top co-authors by number of shared publications:
David Firstbrook
6 shared publicationsPatrick Harkness
5 shared publicationsRyan Timoney
5 shared publicationsDouglas Thomson
Division of Aerospace Sciences, School of Engineering, University of Glasgow, UK
4 shared publications- Euan William McGookin
James Watt School of Engineering University of Glasgow Glasgow UK
4 shared publications - Patrick Harkness
University of Glasgow
4 shared publications
Latest Publications
- Open Access
- 7 February 2024
- Published by Elsevier in Biomedical Signal Processing and Control
- Vol. 92
A cost focused framework for optimizing collection and annotation of ultrasound datasets
- 7 February 2024
- Published by Elsevier in Biomedical Signal Processing and Control
- Vol. 92
Open AccessA cost focused framework for optimizing collection and annotation of ultrasound datasets
- 1 July 2020
- Published by American Society of Civil Engineers (ASCE) in Journal of Aerospace Engineering
- Vol. 33 (4) , 04020040
Development of a Robust Mating System for Use in the Autonomous Assembly of Planetary Drill Strings
Volume-constrained robotic missions seeking to obtain samples from beneath a planetary subsurface may wish to use a rigid drill string consisting of multiple, individual drill bit sections connected together, as opposed to a single, lengthy drill bit. To ensure that drill strings can be assembled and disassembled reliably, it is essential that a robust connection system be used. The authors propose a geometry that seeks to address the requirements of such a mating interface. The proposed solution is based on the bayonet interface, using L- and T-shaped so-called female grooves and male studs connected and disconnected together through a series of clockwise and counterclockwise rotations and single-point clamping events. This routine allows the transfer of both percussion through the drill string and torque in both directions of rotation, while permitting the accurate disconnection of individual drills bits at the required location. Sustained laboratory and field drilling operations suggest that bayonet-style connections offer a reliable solution to the problem of autonomous assembly and disassembly of drill strings in a planetary exploration setting. This paper discusses the development of such a connection system, based on the bayonet connection, which has been implemented in the overall architecture of the Ultrasonic Planetary Core Drill (UPCD). The design trade-off study, which sought to evaluate the use of the bayonet system in comparison with the more conventional screw thread interface, will be discussed, alongside experimental results from percussion transmission testing and drill string assembly testing.
- 1 July 2020
- Published by American Society of Civil Engineers (ASCE) in Journal of Aerospace Engineering
- Vol. 33 (4) , 04020040
Development of a Robust Mating System for Use in the Autonomous Assembly of Planetary Drill Strings
Volume-constrained robotic missions seeking to obtain samples from beneath a planetary subsurface may wish to use a rigid drill string consisting of multiple, individual drill bit sections connected together, as opposed to a single, lengthy drill bit. To ensure that drill strings can be assembled and disassembled reliably, it is essential that a robust connection system be used. The authors propose a geometry that seeks to address the requirements of such a mating interface. The proposed solution is based on the bayonet interface, using L- and T-shaped so-called female grooves and male studs connected and disconnected together through a series of clockwise and counterclockwise rotations and single-point clamping events. This routine allows the transfer of both percussion through the drill string and torque in both directions of rotation, while permitting the accurate disconnection of individual drills bits at the required location. Sustained laboratory and field drilling operations suggest that bayonet-style connections offer a reliable solution to the problem of autonomous assembly and disassembly of drill strings in a planetary exploration setting. This paper discusses the development of such a connection system, based on the bayonet connection, which has been implemented in the overall architecture of the Ultrasonic Planetary Core Drill (UPCD). The design trade-off study, which sought to evaluate the use of the bayonet system in comparison with the more conventional screw thread interface, will be discussed, alongside experimental results from percussion transmission testing and drill string assembly testing.
- 19 December 2018
- Published by Linkoping University Electronic Press
- No. 142,p. 348-355
Numerical Efficiency of Inverse Simulation Methods applied to a Wheeled Rover
Here is information on how to publish, spread your research, and search for your publications. Most of LiU's research publications are directly imported into DiVA from the Web of Science. Before registering a publication, always check if the publication is already in DiVA!
- 19 December 2018
- Published by Linkoping University Electronic Press
- No. 142,p. 348-355
Numerical Efficiency of Inverse Simulation Methods applied to a Wheeled Rover
Here is information on how to publish, spread your research, and search for your publications. Most of LiU's research publications are directly imported into DiVA from the Web of Science. Before registering a publication, always check if the publication is already in DiVA!
- 15 November 2018
- Published by American Society of Civil Engineers (ASCE)
- p. 317-327
Development of a Heuristic Thermal Control System for the Ultrasonic Planetary Core Drill
- 15 November 2018
- Published by American Society of Civil Engineers (ASCE)
- p. 317-327
Development of a Heuristic Thermal Control System for the Ultrasonic Planetary Core Drill
- 15 November 2018
- Published by American Society of Civil Engineers (ASCE)
- p. 297-306
UPCD: Field Trial Results and Further Work
- 15 November 2018
- Published by American Society of Civil Engineers (ASCE)
- p. 297-306
UPCD: Field Trial Results and Further Work
- 15 November 2018
- Published by American Society of Civil Engineers (ASCE)
- p. 359-368
Ultrasonically Assisted Hammer-Action Penetrators in Planetary Regolith
- 15 November 2018
- Published by American Society of Civil Engineers (ASCE)
- p. 359-368
Ultrasonically Assisted Hammer-Action Penetrators in Planetary Regolith
- Open Access
- 1 October 2018
- Published by Institute of Electrical and Electronics Engineers (IEEE)
- p. 1-4
Ultrasonic Auger for Narrow-Gauge Borehole Drilling
An ultrasonic auger was designed, manufactured, and tested in glass microspheres to investigate force and torque reducing effects upon application of high-powered ultrasonic vibration. It was found that whilst vibration had no effect on overhead force during rotary augering, the torque was reduced by up to 30%, depending on amplitude of vibration.
- 1 October 2018
- Published by Institute of Electrical and Electronics Engineers (IEEE)
- p. 1-4
Open AccessUltrasonic Auger for Narrow-Gauge Borehole Drilling
An ultrasonic auger was designed, manufactured, and tested in glass microspheres to investigate force and torque reducing effects upon application of high-powered ultrasonic vibration. It was found that whilst vibration had no effect on overhead force during rotary augering, the torque was reduced by up to 30%, depending on amplitude of vibration.
- 1 September 2018
- Published by Institute of Electrical and Electronics Engineers (IEEE)
- p. 386
Modelling and Control of a Biologically Inspired Trenchless Drilling Device
This work presents the methods used and initial findings of the control of the model for an autonomous trenchless drilling device, with bioinspired worm-like locomotion. The model is validated using Inverse Simulation. The initial control is detailed with data from the simulation and experimental device.
- 1 September 2018
- Published by Institute of Electrical and Electronics Engineers (IEEE)
- p. 386
Modelling and Control of a Biologically Inspired Trenchless Drilling Device
This work presents the methods used and initial findings of the control of the model for an autonomous trenchless drilling device, with bioinspired worm-like locomotion. The model is validated using Inverse Simulation. The initial control is detailed with data from the simulation and experimental device.
- 1 September 2018
- Published by Institute of Electrical and Electronics Engineers (IEEE)
- p. 387
FDIR for a Biologically Inspired Trenchless Drilling Device
Failure Detection, Isolation and Recovery (FDIR) of autonomous systems working in hazardous conditions is essential. Methods of detection and recovery without intervention are required. This work describes the failure modes currently identified with an autonomous biologically inspired trenchless drilling robotic system. Inverse Simulation is used for detecting failures and is demonstrated on a simulation model of the robotic system. Results from the experiments, show that Inverse Simulation can be used to detect and identify system failures.
- 1 September 2018
- Published by Institute of Electrical and Electronics Engineers (IEEE)
- p. 387
FDIR for a Biologically Inspired Trenchless Drilling Device
Failure Detection, Isolation and Recovery (FDIR) of autonomous systems working in hazardous conditions is essential. Methods of detection and recovery without intervention are required. This work describes the failure modes currently identified with an autonomous biologically inspired trenchless drilling robotic system. Inverse Simulation is used for detecting failures and is demonstrated on a simulation model of the robotic system. Results from the experiments, show that Inverse Simulation can be used to detect and identify system failures.
- 1 July 2018
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 55 (4) , 984-992
Autophage Engines: Toward a Throttleable Solid Motor
This paper describes the instrumented test firing of a rocket that seeks to combine the throttleability of a liquid-fueled engine with the simplicity of a solid motor. The concept is that a differentiated fuel and oxidizer rod is forced into a vaporization unit where its constituents transition into separate propellant gases, which are then mixed in a combustion chamber. The vaporization unit is heated by the combustion, and the throttle setting is adjusted by changing the force used to drive the solid propellant rod into the vaporizer, which naturally influences the propellant feed rate. In experiments using a solid propellant rod consisting of polypropylene fuel and a mixture of and oxidizer, operations have been sustained for around 60 s. During testing, using propellant feed forces of between 250 and 900 N, propellant feed rates of between 100 and 300 mm/min have been achieved, which are in turn correlated to chamber pressures of between approximately 300 and 700 kPa. These correlated cycles of control input (the feed force), throttle response (the propellant feed rate), and implied thrust (the chamber pressure) demonstrate, for the first time, a simple solid rocket that can be throttled in real time.- 1 July 2018
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 55 (4) , 984-992
Autophage Engines: Toward a Throttleable Solid Motor
This paper describes the instrumented test firing of a rocket that seeks to combine the throttleability of a liquid-fueled engine with the simplicity of a solid motor. The concept is that a differentiated fuel and oxidizer rod is forced into a vaporization unit where its constituents transition into separate propellant gases, which are then mixed in a combustion chamber. The vaporization unit is heated by the combustion, and the throttle setting is adjusted by changing the force used to drive the solid propellant rod into the vaporizer, which naturally influences the propellant feed rate. In experiments using a solid propellant rod consisting of polypropylene fuel and a mixture of and oxidizer, operations have been sustained for around 60 s. During testing, using propellant feed forces of between 250 and 900 N, propellant feed rates of between 100 and 300 mm/min have been achieved, which are in turn correlated to chamber pressures of between approximately 300 and 700 kPa. These correlated cycles of control input (the feed force), throttle response (the propellant feed rate), and implied thrust (the chamber pressure) demonstrate, for the first time, a simple solid rocket that can be throttled in real time.