Balakrishnan S.N., Tsourdos A., White B.A. Advances in missile guidance, control, and estimation

Automation and Control Engineering. — CRC Press, 2012. — 720 p.
ISBN: 1420083139.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 Estimation brings together in one volume the latest developments in the three major missile-control components — guidance, control, and estimation — as well as advice on implementation. It also shows how these elements contribute to the overall missile design process.Antonios Tsourdos and Brian A. White
Robust Autopilot Design for Quasilinear Parameter-Varying Missile ModelAntonios Tsourdos, Brian A. White, and L. Bruyere
Polynomial Approach for Design and Robust Analysis of Lateral Missile ControlDaniel Alazard
Control Design and Gain Scheduling Using Observer-Based StructuresKarthikeyan Rajagopal and S. N. Balakrishnan
Adaptive Neural Network–Based Autopilot DesignNathan Harl, Michael Dancer, S. N. Balakrishnan, Ernest J. Ohlmeyer,
and C. Phillips
Integrated Guidance and Control for MissilesYuri B. Shtessel and Christian H. Tournes
Higher-Order Sliding Modes for Missile Guidance and ControlPini Gurfil
Neoclassical Missile GuidanceBrian A. White and Antonios Tsourdos
Differential Geometry Applied to Missile GuidanceJosef Shinar and Tal Shima
Differential Game-Based Interceptor Missile GuidanceChang-Kyung Ryoo, Min-Jea Tahk, and Hangju Cho
Optimal Guidance Laws with Impact Angle ControlJosef Shinar and Tal Shima
Integrated Design of Estimator and Guidance LawDavid Salmond
Introduction to Particle Filters for Tracking and GuidancePractical Techniques for the Design of Multirate Digital Guidance Laws and AutopilotsG. Hexner and H. Weiss
Design of CLOS Guidance SystemKevin A. Wise
Practical Considerations in Robust Control of Missiles