Moving mass actuated reentry vehicle control based on trajectory linearization

Engineering

• Aerodynamic Coefficient 100%
• Axisymmetric 33%
• Control Model 33%
• Control System 33%
• Controller Gain 33%
• Flight Control 33%
• Flight Trajectory 33%
• Gain-Scheduling 33%
• Lagrange 33%
• Mass System 33%
• Moving Mass 100%
• Re-Entry Vehicle 66%
• Robust Stability 33%
• Roll Control 33%