Thrust vector V/STOL aircraft control based on angular acceleration estimation

Engineering

• Actuator 33%
• Aircraft Control 100%
• Aircraft Structure 33%
• Angular Acceleration 100%
• Control Vector 33%
• Duct 33%
• Flight Control 33%
• Model Uncertainty 33%
• Moment of Inertia 33%
• Noise Variance 33%
• Non-Linear Dynamics 33%
• Sensor Noise 66%
• Simulation Result 33%
• Stability Analysis 33%
• VTOL/STOL Aircraft 100%