Three-dimensional terminal angle constrained robust guidance law with autopilot lag consideration

Engineering

• Automatic Pilot 100%
• Finite Time 66%
• Simulation Result 33%
• Sliding Mode Control 33%
• Convergent 33%
• Sliding Mode 33%
• Estimation Error 33%
• Design Technique 33%
• Target Manoeuvre 33%
• Design Parameter 33%
• Dimensional Environment 33%