This paper proposes a novel application of differential evolution to solve a difficult dynamic optimisation or optimal control problem. The miss distance in a missile-target engagement is minimised using differential evolution. The difficulty of solving it by existing conventional techniques in optimal control theory is caused by the nonlinearity of the dynamic constraint equation, inequality constraint on the control input and inequality constraint on another parameter that enters problem indirectly. The optimal control problem of finding the minimum miss distance has an analytical solution subject to several simplifying assumptions. In the approach proposed in this paper, the initial population is generated around the seed value given by ...
Differential evolution is arguably one of the hottest topics in today's computational intelligence r...
This dissertation studies the optimal guidance of homing missiles. The guidance objective is to dete...
This dissertation investigates advanced concepts in terminal missile guidance. The terminal phase of...
This paper proposes a novel application of differential evolution to solve a difficult dynamic optim...
This paper proposes a differential evolution based method of improving the performance of convention...
This paper presents a novel, soft computing based solution to a complex optimal control or dynamic o...
Abstract: This paper shows; that, in some conditions we can obtain the exact solution for a missile ...
Kinematics based guidance laws like the proportional navigation (PN) and many other linear optimal g...
Abstract: This paper shows a method to obtain the exact solution for a missile and an aircraft diffe...
This paper describes a missile guidance problem in which the objective is to guide an interceptor mi...
This paper describes a missile guidance problem in which the objective is to guide an interceptor mi...
For complex pursuit-evasion games, a new approach is developed to compute optimal feedback strategie...
In this report the application of the differential game theory to missile guidance problem is consid...
In this paper an optimisation algorithm based on Differential dynamic programming is applied to the ...
Many methods for solving optimal control problems, whether direct or indirect, rely upon gradient in...
Differential evolution is arguably one of the hottest topics in today's computational intelligence r...
This dissertation studies the optimal guidance of homing missiles. The guidance objective is to dete...
This dissertation investigates advanced concepts in terminal missile guidance. The terminal phase of...
This paper proposes a novel application of differential evolution to solve a difficult dynamic optim...
This paper proposes a differential evolution based method of improving the performance of convention...
This paper presents a novel, soft computing based solution to a complex optimal control or dynamic o...
Abstract: This paper shows; that, in some conditions we can obtain the exact solution for a missile ...
Kinematics based guidance laws like the proportional navigation (PN) and many other linear optimal g...
Abstract: This paper shows a method to obtain the exact solution for a missile and an aircraft diffe...
This paper describes a missile guidance problem in which the objective is to guide an interceptor mi...
This paper describes a missile guidance problem in which the objective is to guide an interceptor mi...
For complex pursuit-evasion games, a new approach is developed to compute optimal feedback strategie...
In this report the application of the differential game theory to missile guidance problem is consid...
In this paper an optimisation algorithm based on Differential dynamic programming is applied to the ...
Many methods for solving optimal control problems, whether direct or indirect, rely upon gradient in...
Differential evolution is arguably one of the hottest topics in today's computational intelligence r...
This dissertation studies the optimal guidance of homing missiles. The guidance objective is to dete...
This dissertation investigates advanced concepts in terminal missile guidance. The terminal phase of...