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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
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Design, Construction and Type Certificate The following chapter covers the initial design, construction, registration and test flying of the first prototype of a new aircraft.
A trimmed flight condition is perhaps best thought of as an equilibrium condition. The simplest trim condition is straight-and-level flight, in which the forces (weight, propulsive
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