Finite-Time guidance and control for uncrewed receiver aircraft in aerial refueling rendezvous

Engineering

• Flight Control 100%
• Finite Time 100%
• Control System 33%
• Parameter Uncertainty 33%
• Vortex 33%
• Relative Position 33%
• Sliding Mode 33%
• Control Scheme 33%
• Prescribed Performance 33%
• Guidance System 33%
• Sliding-Mode Controller 33%
• Target Point 33%
• Rendezvous Guidance 33%