AN IMPROVED GUIDANCE ALGORITHM FOR SOLID PROPELLENT BALLISTIC MISSILES

On-line Control Technique for Missile Autopilot

NEAR OPTIMAL GUIDANCE FOR SHORT RANGE HOMING MISSILE,USING THE MINIMAL ORDER OBSERVER

Advanced top-attack trajectory guidance law with impact angle

Modeling and Simulating Guidance Laws for Gun-Launched Guided Munitions

Trajectory Prediction for a Typical Fin Stabilized Artillery Rocket

Trajectory Modeling of GRAD Rocket with Low-Cost Terminal Guidance Upgrade Coupled to Range Increase Through Step-Like Thrust-Curves

Classical Autopilot Design for a Semiactive Homing Guided Missile

Design and Implementation of Digital Missile Trajectory Controller

Performance Enhancement of a Long Range Missile Using HoRobust Control Design