Missile guidance refers to a variety of methods of guiding a missile or a guided bomb to its intended target.

This requires great precision and very fast response from the missile airframe. 1. J. Shinar , I. In the view of the recently acknowledged need for improved guidance laws the differential game formulation has a substantial advantage. 1). 1. Forte and B. Kantor ; 23 May 2012 | Journal of Guidance, Control, and Dynamics, Vol. The missile's target accuracy is a critical factor for its effectiveness. Mixed strategy guidance - A new high-performance missile guidance law. Integrated Guidance and Control for Homing Missiles Neil F. Palumbo, Brian E. Reardon, and Ross A. Blauwkamp he need to engage and negate highly maneuverable threats imposes stringent per-formance requirements on missile interceptors. Discrete optimal guidance for high-order missile and maneuvering target. IEEE Transactions on Aerospace and Electronic Systems, Vol. 28, No. Design of a CLOS guidance law via feedback linearization. The guidance algorithm issues command to the autopilot to enable the missile to be guided onto the target. In addition to these guidance systems, two other forms of missile guidance have been used in the past or are being used presently: (a) inertial guidance (used mostly in ballistic missiles, and which will be discussed in detail in a later chapter), and (b) position-fixing guidance. loop, represents an essential component in the design The demands on the missile acceleration capability, of guided missile system's2 (Fig. In this paper we present the current trends on missile guidance systems design. Some guided missiles may contain combinations of the above systems.

Guidance systems improve missile accuracy by improving its Probability of Guidance (Pg). Missile Guidance Law Based on Robust Model Predictive Control Using Neural-Network Optimization Abstract: In this brief, the utilization of robust model-based predictive control is investigated for the problem of missile interception. In spite of the results of this comparison, and a subsequent paper advocating this approach for guidance law synthesis of future interceptor missiles (Shinar, 1989), differential game guidance laws have not yet been adopted by the missile industry. This process is experimental and the keywords may be updated as the learning algorithm improves. 17, No. Missile Guidance Proportional Navigation Closing Velocity Command Guidance Target Maneuver These keywords were added by machine and not by the authors. The guidance law, as part of the guidance of necessary sensors and information processing.