This study applies deep-reinforcement-learning algorithms to integrated guidance and control for three-dimensional, high-maneuverability missile-target interception. Dynamic environment, reward functions concerning multi-factors, agents based on the deep-deterministic-policy-gradient algorithm, action signals with pitch yaw fins as commands were constructed in research, which missile order inte...

This paper investigates the application of velocity-based gain-scheduling techniques to a demanding, highly nonlinear, missile control design task. Scheduling on instantaneous incidence (a rapidly varying quantity) is well known to lead to considerable difficulties with conventional gain-scheduling methods. Moreover, the missile dynamics do not have well-defined relative degree at operating poi...

In this literature, a data pre-processing circuit designs and analyses for an infrared image seeker of a subsonic cruise missile are proposed. The flight speed of the missile is 250m/s. Therefore, automatic contrast control and automatic brightness control are usually needed to keep wanted contrast and brightness for best image properties in target recognition and tracking; especially for the m...

Human-agent interaction for learning with instruction can be viewed on a continuum of instructor/agent control. At one extreme are systems that learn by instructor-driven interactions, such as learning by demonstration, examples, or imitation. The other extreme of the continuum is occupied by systems where instructor interaction is limited to responding to the questions posed by the agent or to...

High-level networking model and technology suitable for effective management of large distributed dynamic air and missile defense systems will be described which can cope with different kinds of unpredictable and asymmetric situations including massive air and missile attacks. Using this Spatial Grasp Technology (SGT), intelligent distributed command and control infrastructures, as demonstrated...

Abstract The design of guidance law for smart missile based on implicit dynamic-inverse direct mode configuration is described in this paper. theory and algorithm are applied to the law. pitching acceleration yaw designed pitch channel by using augmented proportional respectively. attacking time parameter attack error equation introduced as constraint criteria dynamic-inverse. According singula...

Abstract This paper introduces a design method of hardware-in-the-loop simulation system applied to certain type image-guided missile. By studying the characteristics missile, working principle image-guidance is analyzed, mathematical scheme and are designed, mechanism RTX analyzed. Established real-time based on RTX+Windows, analyzed delay computer, simulated launch control flight motion simul...

The traditional approach to improving the lethality of a missile has been to concentrate efforts in the guidance and control systems to improve accuracy and agility. In this paper, we consider how optimizing the endgame, the final few milliseconds before detonation, can yield improvements in overall lethality. As there is likely to be uncertainty in both the target parameters and missile coordi...