Simulation models to study the effects of the pitch control augmentation system on the stability of the F-18 fighter aircraft

An edition of Simulation models to study the effects of the pitch control augmentation system on the stability of the F-18 fighter aircraft (1987)

Simulation models to study the effects of the pitch control augmentation system on the stability of the F-18 fighter aircraft

By J. L. Denis Lamanque

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Publish Date

1987

Publisher

Royal Military College of Canada

Language

Pages

Description:

subjects: Stability, F-18 aircraft, Pitch