Missile Motion Sensitivity to Dynamic Stability Derivatives
Final rept. 1 Oct 1978-30 Sep 1979
ARNOLD ENGINEERING DEVELOPMENT CENTER ARNOLD AFB TN
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A dynamic derivative sensitivity study was conducted to demonstrate the importance of dynamic derivatives in missile motion simulation studies. Generalized bank-to-turn and yaw-to-turn missile configurations were used with a six-degree-of-freedom linearized stability program. The effects of various dynamic derivatives on missile stability were investigated in both level and turning flight for several Mach numbers and altitude conditions.
- Numerical Mathematics
- Guided Missile Dynamics, Configurations and Control Surfaces
- Fluid Mechanics