| Titre : | Missile Guidance System Design Using Optimal Control | | Type de document : | document multimédia | | Auteurs : | Abderaouf Taleb, Auteur ; Salah Eddine Benhorma, Auteur ; Lakhdar Mokrani, Directeur de thèse | | Editeur : | Laghouat : Université Amar Telidji - Département d'électrotechnique | | Année de publication : | 2023 | | Importance : | 120p. | | Accompagnement : | CD ROM Optique | | Note générale : | Option: Automation and Systems
| | Langues : | Français | | Mots-clés : | Missile modeling, 6DOF model, 3DOF model, Guidance system, LQR optimal. control, Moving and maneuvering target, Simulation results, Optimal guidance law performance. | | Résumé : | The aim of this memoir work is to develop a Linear Quadratic Regulator (LQR) optimal control law that minimizes a performance index ‘or cost functional’ in order to perform an effective and accurate intercept guidance system of a three Degrees Of Freedom (3DOF) guided missile. First of all, a state of the art review, that concerns mainly missiles types and
launch modes, propulsion and guidance systems, and commonly used optimal control methods used in guided missiles, has been established. Then, the missile 6DOF and 3DOF motion modeling has been performed by determining both velocity components and rotation rates dynamic expressions in body-fixed and inertial frames. Next, the LQR optimal control
method has been presented and used to get the most favorable intercept guidance law in order to ensure an accurate and effective missile-target tracking and hitting. Finally, simulation results have been presented and discussed to study the dynamics of an open loop 6DOF missile model and show the aptitude of the performed optimal control law of a 3DOF missile guidance system to track and hit a fast moving and maneuvering target.
| | note de thèses : | Memoire de Master en Electrotechnique |
Missile Guidance System Design Using Optimal Control [document multimédia] / Abderaouf Taleb, Auteur ; Salah Eddine Benhorma, Auteur ; Lakhdar Mokrani, Directeur de thèse . - Laghouat : Université Amar Telidji - Département d'électrotechnique, 2023 . - 120p. + CD ROM Optique. Option: Automation and Systems
Langues : Français | Mots-clés : | Missile modeling, 6DOF model, 3DOF model, Guidance system, LQR optimal. control, Moving and maneuvering target, Simulation results, Optimal guidance law performance. | | Résumé : | The aim of this memoir work is to develop a Linear Quadratic Regulator (LQR) optimal control law that minimizes a performance index ‘or cost functional’ in order to perform an effective and accurate intercept guidance system of a three Degrees Of Freedom (3DOF) guided missile. First of all, a state of the art review, that concerns mainly missiles types and
launch modes, propulsion and guidance systems, and commonly used optimal control methods used in guided missiles, has been established. Then, the missile 6DOF and 3DOF motion modeling has been performed by determining both velocity components and rotation rates dynamic expressions in body-fixed and inertial frames. Next, the LQR optimal control
method has been presented and used to get the most favorable intercept guidance law in order to ensure an accurate and effective missile-target tracking and hitting. Finally, simulation results have been presented and discussed to study the dynamics of an open loop 6DOF missile model and show the aptitude of the performed optimal control law of a 3DOF missile guidance system to track and hit a fast moving and maneuvering target.
| | note de thèses : | Memoire de Master en Electrotechnique |
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Missile Guidance System Design Using Optimal Control
