Lateral acceleration control design of a non-linear homing missile using multi-objective evolution strategies

T Sreenuch, A Tsourdos, EJ Hughes… - … 2004 American control …, 2004 - ieeexplore.ieee.org
… Absnnct-The paper presents the lateral acceleration control design of non-linear missile
the application of multi-objective evolutionary optimization to a robust autopilot design. The aim …

Lateral acceleration control design of a non-linear homing missile using multi-objective evolutionary optimisation

T Sreenuch, A Tsourdos, BA White… - … on Evolutionary …, 2003 - ieeexplore.ieee.org
lateral acceleration control design of non-linear missile model using a multiobjective
evolutionary … The controller design for the uncertain plants is carried out by minimising gain and …

Nonlinear model-predictive integrated missile control and its multiobjective tuning

V Bachtiar, C Manzie, EC Kerrigan - Journal of Guidance, Control, and …, 2017 - arc.aiaa.org
… dvanced missile control designs have been founded on recent developments aimed at a
more streamlined engineering design approach to improve performance and the cost of design. …

Multi-Objective Frequency Loop-Shaping of a Lateral Missile Autopilot

T Sreenuch, A Tsourdos, EJ Hugbes… - IFAC Proceedings Volumes, 2004 - Elsevier
… the lateral acceleration control design of non-linear missile model using the multi-objective
evolutionary … Basic scheme of the multi-objective evolution strategy «(JL + '\)-ES) used in this …

Fuzzy gain-scheduled missile autopilot design using evolutionary algorithms

T Screenuch, A Tsourdos, EJ Hughes… - IEEE Transactions on …, 2006 - ieeexplore.ieee.org
… the Pareto front can be identified using the evolution strategy (ES) as … A multi-objective
selection procedure used in this study is as … in lateral acceleration control design of missiles using

[HTML][HTML] Optimization of three-loop missile autopilot gain under crossover frequency constraint

MA Abd-Elatif, L Qian, Y Bo - Defence Technology, 2016 - Elsevier
… In a different way, the multi-objective optimization technique is … design of a typical missile
system using the proposed technique, and the results are compared with the design strategy of …

An artificial delay based robust guidance strategy for an interceptor with input saturation

A Banerjee, J Mukherjee, M un Nabi, IN Kar - ISA transactions, 2021 - Elsevier
… The design of non-linear control methods for missiles to intercept targets, have been the …
A missile is designed to withstand a limited magnitude of lateral acceleration or latax while …

[BOOK][B] Advanced tracking strategies for linear and nonlinear control systems: Theory and applications

AMA Khamis - 2014 - search.proquest.com
design for a homing ballistic missile intercept problem using … The extension of the analytical
multi-objective parameter synthesis … design of nonlinear controllers, very common within the …

[PDF][PDF] Constrained-Optimal Based Loop-Shaping State Feedback Approach for Missile Autopilot Design

MA Abd-Elatif, Q Longjun, B Yuming - International Journal of Modeling and …, 2016 - ijmo.org
… As a result, the flight control design of a missile system is a creative process as it considers
both performance requirements and performance limitations, which are inherently conflicting. …

Identification of a non-linear hydraulic actuator considering rate saturation using particle swarm optimisation algorithm

P Sarhadi, NO Ghahramani… - … and Control, 2013 - inderscienceonline.com
… In this paper, non-linear model of a hydraulic actuator … -order transfer function and non-linear
functions of saturation with … , unknown parameters of the non-linear model are estimated. As …