Observer-based robust high-order fully actuated attitude autopilot design for spinning glide-guided projectiles

Engineering

• Automatic Pilot 100%
• Feedback Control System 66%
• Computer Simulation 33%
• External Disturbance 33%
• Sliding Mode 33%
• Non-Linear Dynamic 33%
• Total Disturbance 33%
• Initial Condition 33%
• Model Uncertainty 33%
• Lyapunov Methods 33%