In this paper, the stable region for missile guidance loop employing an integrated proportional navigation guidance law is derived. The missile guidance loop is formulated as a closed-loop control system consisting of a linear time-invariant feed-forward block and a time-varying feedback gain. By applying the circle criterion to the system, a bound for the time of flight up to which stability c...

The main problem in bringing autonomy to any vehicle lies in the design of a suitable guidance law. For a truly autonomous operation, the vehicle needs to have a reliable Navigation, Guidance and Control (NGC) system of which the guidance system is the key element, which generates suitable trajectories to be followed. In this survey paper, various guidance laws found in the literature and their...

Abstract The vehicle-mounted missile vertical thermal emission not only has excellent maneuverability, randomness, and concealment, but also a short response time, good versatility, high reliability, so it is widely used. In order to explore the gas flow field of missile, firstly, this study introduces theoretical basis deep reinforcement learning (DRL) algorithm wireless sensor network (WSN). ...

–A flight path rate demand modified three-loop lateral missile autopilot design methodology for a class of guided missile, based on state feedback, output feedback, reduced order Das & Ghosal observer (DGO) is proposed. The open loop undamped model of three-loop autopilot has been stabilized by using pole placement and state feedback. The non-minimum phase feature of rear controlled missile air...

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...