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Flight dynmaics
The study of aircraft- Stability & Trim (Equilibrium)- Motion due to
• Control inputs
• Atmospheric Disturbances
• We will consider for the most part fixed-wing aircraft
• Subject builds on
- Mechanics (Statics & Dynamics)
- Aerodynamics
- Contro
Specify the inner-loop gain such that the damping coefficient of the closed loop is equal to 0.4
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