Advances in Missile Guidance, Control, and Estimation

Stringent demands on modern guided weapon systems require new approaches to guidance, control, and estimation. There are requirements for pinpoint accuracy, low cost per round, easy upgrade paths, enhanced performance in counter-measure environments, and the ability to track low-observable targets. Advances in Missile Guidance, Control, and Estimat

A. Tsourdos, S.N. Balakrishnan, B.A. White

Robust Autopilot Design for Quasilinear Parameter-Varying Missile Model. Polynomial Approach for Design and Robust Analysis of Lateral Missile Control. Control Design and Gain Scheduling Using Observer-Based Structures. Adaptive Neural Network-Based Autopilot Design. Integrated Guidance and Control for Missiles. Higher-Order Sliding Modes for Missile Guidance and Control. Neoclassical Missile Guidance. Differential Geometry Applied to Missile Guidance. Differential Game-Based Interceptor Missile Guidance. Practical Techniques for the Design of Multirate Digital Guidance Laws and Autopilots. Optimal Guidance Laws with Impact Angle Control. Integrated Design of Estimator and Guidance Law. Introduction to Particle Filters for Tracking and Guidance. Design of CLOS Guidance System. Practical Considerations in Robust Control of Missiles. Index.