An Online Optimal Explicit Guidance Scheme for Long Range Missiles with Solid Motors

MICROPROCESSOR IMPLEMENTATION OF AN ON-LINE OPTIMAL ESTIMATOR OF GUIDANCE STATES FOR A SHORT-RANGE HOMING SYSTEM

Classical Autopilot Design for a Semiactive Homing Guided Missile

CONTROL SYSTEM DESIGEN TECHNIQUES FOR GUIDED MISSILES

Short Range Missile Autopilot Design using Fuzzy Control Technique

Advanced top-attack trajectory guidance law with impact angle

Derivation of Optimal Guidance and Control Problem

AN IMPROVED GUIDANCE ALGORITHM FOR SOLID PROPELLENT BALLISTIC MISSILES

Performance Evaluation of Homing Guidance Methods

On-line Control Technique for Missile Autopilot