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James Dyer

dblp:42/5701 · DBLP profile ↗
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3ranked-venue papers
3as first author
0since 2021 · last 2019
0000-0002-0617-8817ORCID · corroborated

Domains — the database's venue-derived domains; a paper can count in several

Security and privacy · 2 · 2 first-authorApplied, interdisciplinary, general and emerging computing · 1 · 1 first-author

Expertise — from the expertise taxonomy: the topics of the expert's papers under the CCF categories. A weight counts papers with recency: 1 for a paper about the topic, 0.3 when the topic is its context, halved every five years.

Interdisciplinary, comprehensive, and emerging computing
1 paper
Computational science and engineering · 100%

Topics — the 2 heaviest of 2, each with the papers that count most for it

TopicWeightPapersLastEvidence papers
Computational science and engineering › numerical solution of differential equations
multistep methods		 0.011968
Generalized Multistep Methods in Satellite Orbit Computation · J. ACM 1968
Computational science and engineering
numerical analysis		 0.011968
Generalized Multistep Methods in Satellite Orbit Computation · J. ACM 1968

Methods — techniques the papers use, named apart from their topics

quasi-hermite interpolating polynomials · 0.0generalized multistep methods · 0.0
YearPublicationVenuePosition
2019 Order-preserving encryption using approximate common divisors
James Dyer, Martin E. Dyer, Karim Djemame
 J. Inf. Secur. Appl.1
2017 Practical Homomorphic Encryption Over the Integers for Secure Computation in the Cloud
James Dyer, Martin E. Dyer, Jie Xu 0007
 IMACC1
1968 Generalized Multistep Methods in Satellite Orbit Computation
abstract
The theory of generalized multistep methods using an off-grid point is extended to the special second-order equation y″ = f ( x , y ). New high-order methods for solving this equation, based on quasi-Hermite interpolating polynomials, are shown to exist, as well as new explicit generalized methods for a first-order equation. Some results in the theory of quasi-Hermite interpolation are given, and results of computations of an unperturbed orbit trajectory are presented.
James Dyer
 J. ACM1