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Journal ArticleDOI

Cooperative Strategies for Optimal Aircraft Defense from an Attacking Missile

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This article is published in Journal of Guidance Control and Dynamics.The article was published on 2015-04-08. It has received 94 citations till now. The article focuses on the topics: Missile & Air-to-air missile.

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Fault-Tolerant Cooperative Control of Multiagent Systems: A Survey of Trends and Methodologies

TL;DR: A survey of trends and methodologies of fault tolerant cooperative control in multiagent systems finds that multiple agents can provide much more redundancy than a single agent system, thereby making the fault tolerance cooperative control design more flexible.
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A differential game for cooperative target defense

TL;DR: A barrier based on the explicit policy method and geometric analysis method is constructed to separate the whole state space into two disjoint parts that correspond to two winning regions for the Attacker and Target–Defender team.
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Design and Analysis of State-Feedback Optimal Strategies for the Differential Game of Active Defense

TL;DR: This paper provides a complete, closed form solution of the active target defense differential game; synthesize closed-loop state feedback optimal strategies for the agents and obtain the Value function of the game.
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Cooperative Nonlinear Guidance Strategies for Aircraft Defense

TL;DR: In this article, the authors present nonlinear guidance strategies for scenarios where an aircraft launches a defender missile as a countermeasure against an incoming attacking missile, and design of guidance strategies is performed in a nonlinear framework, using sliding-mode control technique, with relevant zero-effort miss variables as switching surfaces.
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Cooperative Missile Guidance for Active Defense of Air Vehicles

TL;DR: This paper discusses the case where the Defender is endowed with a positive capture radius and a differential game is presented where the Target–Defender team strives to maximize the terminal separation between the Target and the Attacker at the time instant where the attacker is intercepted by the Defender.
References
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Optimal Control Theory

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.
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Cooperative Multiple-Model Adaptive Guidance for an Aircraft Defending Missile

TL;DR: In this article, a cooperative guidance law for a defender missile protecting an aerial target from an incoming homing missile is presented, where the defender knows the future evasive maneuvers to be performed by the protected target and thus can anticipate the maneuvers it will induce on the incoming Homing missile.
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Line-of-Sight Interceptor Guidance for Defending an Aircraft

TL;DR: In this paper, the authors defined the following components of an evasive maneuver component normal to the target-missile line of sight: amp, ad, am, target, defender, and missile lateral accelerations, respectively at max, ad max, am max, max, and am max = target, defenders, and missiles maximum lateral acceleration.
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Defending a Moving Target Against Missile or Torpedo Attack

TL;DR: In this paper, the authors derived the kinematic relations among the three bodies (missile, target, and counter-weapon) in closed form under the asymptotic approximation of constant-bearing trajectories (collision courses).
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