On parameter uniform and layer resolving numerical method for a singularly perturbed model in aerodynamics

In this paper, a parameter uniform computational technique is examined for a partially singularly perturbed semi-linear system of equations which models the flight dynamics of an Unmanned Aerial Vehicle (UAV) and a Helicopter. The components of the solution of this system are expected to exhibit ove...

Full description

Bibliographic Details
Main Authors: K. Saravana Sankar, L. Jones Tarcius Doss
Format: Article
Language:English
Published: Elsevier 2023-03-01
Series:Results in Control and Optimization
Subjects:
Online Access:http://www.sciencedirect.com/science/article/pii/S2666720723000103