Analytic Approach and Landing Guidance through a Novel Time-Varying Sliding Mode Control Method

Engineering

• Computer Simulation 50%
• Finite Time 50%
• First Order Linear Differential Equation 50%
• Flight Path Angle 50%
• Normal Load Factor 50%
• Reference Trajectory 50%
• Reusable Launch Vehicle 100%
• Sliding Mode Control 100%
• System State 100%