Zobrazeno 1 - 10
of 61
pro vyhledávání: '"Jimoh O Pedro"'
Publikováno v:
Journal of Low Frequency Noise, Vibration and Active Control, Vol 39 (2020)
Resolving the trade-offs between suspension travel, ride comfort, road holding, vehicle handling and power consumption is the primary challenge in the design of active vehicle suspension system. Multi-loop proportional + integral + derivative control
Externí odkaz:
https://doaj.org/article/8a1c2077703c4f93bd81409cb832f118
Publikováno v:
SN Applied Sciences, Vol 4, Iss 4, Pp 1-19 (2022)
Abstract A direct adaptive sliding mode controller (SMC) based on radial basis function neural network (RBFNN) approximation is proposed for a high-speed, ultratall building elevator system using genetic algorithm (GA) to optimise the control paramet
Externí odkaz:
https://doaj.org/article/bf077bcc59b749cca02510322a808b0e
Publikováno v:
International Journal of Dynamics and Control. 10:1903-1921
Publikováno v:
IFAC-PapersOnLine. 54:204-209
Publikováno v:
IFAC-PapersOnLine. 53:14438-14443
This paper presents the design of a particle swarm-optimised model predictive controller (MPC) for a half-car nonlinear electrohydraulic suspension system as it traverses a deterministic road disturbance. The particle swarm optimisation (PSO) algorit
Autor:
Chioniso Kuchwa-Dube, Jimoh O. Pedro
Publikováno v:
Control Engineering Practice. 127:105284
Autor:
Lindokuhle J. Mpanza, Jimoh O. Pedro
Publikováno v:
Algorithms
Volume 14
Issue 6
Algorithms, Vol 14, Iss 178, p 178 (2021)
Volume 14
Issue 6
Algorithms, Vol 14, Iss 178, p 178 (2021)
This paper presents the parameter optimisation of the flight control system of a singlerotor medium-scale rotorcraft. The six degrees-of-freedom (DOF) nonlinear mathematical model of the rotorcraft is developed. This model is then used to develop pro
Autor:
Lindokuhle J. Mpanza, Jimoh O. Pedro
Publikováno v:
2020 3rd International Conference on Control and Robots (ICCR).
The move towards lighter, modular and more energy efficient transportation has led to the development of “more electrical” system. In this paper, the description of an electromechanical actuator (EMA) for flight control applications is presented.
Application of Two Time-Scale Separation NDI Controller to a Dual Aerodynamically-Controlled Missile
Publikováno v:
ANZCC
Agile dual aerodynamically-controlled (DAC) missile presents a sophisticated flight control problem given the inherent missile-nonlinear and tail-fin-canard coupling dynamics that render the system non-affine in control. Given the complexity of the p
Autor:
Jimoh O. Pedro, Paulin Kantue
Publikováno v:
ICSTCC
An integrated approach to the fault detection and diagnosis (FDD) of an unmanned aerial vehicle is presented. A novel approach using the Time Difference Of Arrival (TDOA) principle has been developed to detect, isolate and identify an incipient fault