Path following of optimal trajectories using preview control

Keyphrases

• Optimal Preview Control 100%
• Preview Control 100%
• Surface-to-air Missile 50%
• Missile Model 50%
• Missile Dynamics 50%
• Guidance Trajectory 50%
• Acquisition Range 50%
• Reference Trajectory 50%
• Guidance Loop 50%
• Preview Controller 50%
• Tracking Trajectory 50%

Engineering

• Missile Dynamics 33%
• Reference Trajectory 33%
• Preview Length 33%