Finite-Horizon Optimal Tracking Guidance for Aircraft Based on Approximate Dynamic Programming

Engineering

• Flight Path Angle 100%
• Finite Horizon 100%
• Dynamic Programming 100%
• Feedback Control 50%
• Square Method 50%
• Least Square 50%
• Gauss 50%
• Control Parameter 50%
• Cost Function 50%
• Flight Altitude 50%
• Reference Trajectory 50%
• Conventional Time 50%
• Kinematic Model 50%
• Small-Perturbation Theory 50%
• Critic Network 50%
• Dynamic Programming Method 50%