
<abstract><p>This paper presents and examines a newly improved linear technique for solving the equilibrium problem of a pseudomonotone operator and the fixed point problem of a nonexpansive mapping within a real Hilbert space framework. The technique relies two modified mildly inertial methods and the subgradient extragradient approach. In addition, it can be viewed as an advancement over the previously known inertial subgradient extragradient approach. Based on common assumptions, the algorithm's weak convergence has been established. Finally, in order to confirm the efficiency and benefit of the proposed algorithm, we present a few numerical experiments.</p></abstract>
Aerospace Engineering, FOS: Mechanical engineering, Nonlinear Operators, Fixed-Point Problems, Mathematical analysis, Engineering, Interior-Point Methods, subgradient extragradient, QA1-939, FOS: Mathematics, Classical mechanics, equilibrium problem, Subgradient method, Numerical Analysis, Numerical Optimization Techniques, fixed point problem, Equilibrium Problems, Physics, Mathematical optimization, Iterative Algorithms for Nonlinear Operators and Optimization, Fixed point, Applied mathematics, Computational Theory and Mathematics, mildly inertial, Computer Science, Physical Sciences, Inertial frame of reference, Autonomous Aerial Refueling Systems for UAVs, Mathematics, Mixed-Integer Nonlinear Programs
Aerospace Engineering, FOS: Mechanical engineering, Nonlinear Operators, Fixed-Point Problems, Mathematical analysis, Engineering, Interior-Point Methods, subgradient extragradient, QA1-939, FOS: Mathematics, Classical mechanics, equilibrium problem, Subgradient method, Numerical Analysis, Numerical Optimization Techniques, fixed point problem, Equilibrium Problems, Physics, Mathematical optimization, Iterative Algorithms for Nonlinear Operators and Optimization, Fixed point, Applied mathematics, Computational Theory and Mathematics, mildly inertial, Computer Science, Physical Sciences, Inertial frame of reference, Autonomous Aerial Refueling Systems for UAVs, Mathematics, Mixed-Integer Nonlinear Programs
| selected citations These citations are derived from selected sources. This is an alternative to the "Influence" indicator, which also reflects the overall/total impact of an article in the research community at large, based on the underlying citation network (diachronically). | 1 | |
| popularity This indicator reflects the "current" impact/attention (the "hype") of an article in the research community at large, based on the underlying citation network. | Average | |
| influence This indicator reflects the overall/total impact of an article in the research community at large, based on the underlying citation network (diachronically). | Average | |
| impulse This indicator reflects the initial momentum of an article directly after its publication, based on the underlying citation network. | Average |
