Investigation of Reusable Launch Vehicle Landing Guidance Control with Multiple Sliding Surface Technique

Engineering

• Boundary Condition 33%
• Closed Loop 33%
• Convergent 33%
• Finite Time 33%
• Global Stability 33%
• Initial Condition 33%
• Reusable Launch Vehicle 100%
• Sliding Mode Control 33%
• Sliding Surface 100%

Computer Science

• Boundary Condition 50%
• Initial Condition 50%
• lyapunov theory 50%
• Sliding Mode Control 50%
• Sliding Surface 100%

Physics

• Boundary Condition 33%
• Reusable Launch Vehicle 100%