T
Tal Shima
Researcher at Technion – Israel Institute of Technology
Publications - 185
Citations - 5596
Tal Shima is an academic researcher from Technion – Israel Institute of Technology. The author has contributed to research in topics: Missile & Missile guidance. The author has an hindex of 36, co-authored 176 publications receiving 4738 citations. Previous affiliations of Tal Shima include Air Force Research Laboratory & Rafael Advanced Defense Systems.
Papers
More filters
Journal ArticleDOI
Sliding-Mode Control for Integrated Missile Autopilot Guidance
TL;DR: In this paper, a sliding-mode controller is derived for an integrated missile autopilot and guidance loop, motivated by a differential game formulation of the guidance problem, a single sliding surface, defined using the zero-effort miss distance, is used.
Journal ArticleDOI
Multiple task assignments for cooperating uninhabited aerial vehicles using genetic algorithms
TL;DR: Monte Carlo simulations demonstrate the viability of the genetic algorithm by showing that it consistently and quickly provides good feasible solutions, which makes the real time implementation for high-dimensional problems feasible.
Journal ArticleDOI
Linear Quadratic Guidance Laws for Imposing a Terminal Intercept Angle
Vitaly Shaferman,Tal Shima +1 more
TL;DR: In this article, the authors derived linear quadratic guidance laws that explicitly enable imposing a predetermined intercept angle for arbitrary-order linear missile dynamics, which are dependent on the well-known zero-effort miss distance and on a new variable denoted zeroeffort angle.
Journal ArticleDOI
Optimal Cooperative Pursuit and Evasion Strategies Against a Homing Missile
TL;DR: It is shown how the target can lure in the attacker, allowing its defender to intercept the attacking missile even in scenarios in which the defender's maneuverability is at a disadvantage compared with the attacking ballistic missile.
Journal ArticleDOI
Cooperative Differential Games Strategies for Active Aircraft Protection from a Homing Missile
TL;DR: In this paper, a linear quadratic differential game formulation for arbitrary-order linear players' dynamics in the continuous and discrete domains is derived for a team composed of two agents, where the target aircraft performs evasive maneuvers and launches a defending missile to intercept the homing missile.