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.
Publisher: Royal Military College of Canada
Published: 1987
Place of publication: Kingston, Ont
Subjects: F-18 aircraft; Pitch; Stability
Notes: Thesis (M. Eng. )-Royal Military College of Canada, 1987.

Includes bibliographical references: p. 202-207.