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Aircraft Motion Sensitivity to Cross and Cross-coupling Damping Derivatives

R. W. Butler

出版	Arnold Engineering Development Center, Propulsion Wind Tunnel Facility, Air Force Systems Command, United States Air Force, 1976
URL	http://books.google.com.hk/books?id=ePxSwDQiBvwC&hl=&source=gbs_api

註釋

An investigation was conducted to provide some insight into the importance of dynamic cross and cross-coupling derivatives in motion simulation studies of fighter aircraft in the maneuvering flight regime. The aircraft motion sensitivity to the various derivatives is ascertained in level and turning flight utilizing a 5 deg of freedom linearized stability program. The results are presented in a root locus format.