University of Minnesota M.S. thesis. May 2010. Major: Aerospace Engineering and Mechanics. Advisor: Prof. Gary J. Balas. 1 computer file (PDF); xv, 91 pages, appendix A.The F/A-18 Hornet aircraft with the original flight control law exhibited an out-of-control phenomenon known as the falling leaf mode. The falling leaf mode went undetected during the validation and verification stage of the flight control law. Several F/A-18 Hornet aircraft were lost due to the falling leaf mode and this led NAVAIR and Boeing to redesign the flight control law. The revised flight control law exhibited successful suppression of the falling leaf mode during flight tests with aggressive maneuvers. Prior to performing expensive flight tests, the flight control ...
The realm of aircraft flight dynamics analysis reaches from local static stability to global dynamic...
The successful high angle of attack (HAOA) operation of fighter aircraft will necessarily require th...
Current practice for flight control validation relies heavily on linear analyses and nonlinear, high...
The F/A-18 Hornet aircraft with the original flight control law exhibited a nonlinear out-of-control...
The F/A-18 Hornet aircraft with the original flight control law exhibited a nonlinear out-of-control...
Summary. The current practice to validate flight control laws relies on applying linear analysis too...
F / A - 18 Hornet aircraft is prone to nonlinear phenomenon known as the fulling leaf mode, which w...
The implementation of Flight Control Law (FCL) for Aircraft Electronic Flight Control System (EFCS) ...
A large-angle simulation model for the F-18C/D has been recently validated and reported.1-11 Utilizi...
This thesis analyzes the recent Version 10.7 Operational Flight Program (v10.7 OFP) Flight Control S...
Thesis (Master's)--University of Washington, 2020This work addresses control law synthesis for activ...
This thesis deals with high angle of attack behaviour of a generic delta wing model aircraft. A high...
This dissertation seeks to tackle the aircraft loss-of-control problem by adaptive backup flight con...
In the design of °ight control system modeling uncertainties in the form of param-eter variations is...
This work addresses control law synthesis for active flutter suppression followed by the design and ...
The realm of aircraft flight dynamics analysis reaches from local static stability to global dynamic...
The successful high angle of attack (HAOA) operation of fighter aircraft will necessarily require th...
Current practice for flight control validation relies heavily on linear analyses and nonlinear, high...
The F/A-18 Hornet aircraft with the original flight control law exhibited a nonlinear out-of-control...
The F/A-18 Hornet aircraft with the original flight control law exhibited a nonlinear out-of-control...
Summary. The current practice to validate flight control laws relies on applying linear analysis too...
F / A - 18 Hornet aircraft is prone to nonlinear phenomenon known as the fulling leaf mode, which w...
The implementation of Flight Control Law (FCL) for Aircraft Electronic Flight Control System (EFCS) ...
A large-angle simulation model for the F-18C/D has been recently validated and reported.1-11 Utilizi...
This thesis analyzes the recent Version 10.7 Operational Flight Program (v10.7 OFP) Flight Control S...
Thesis (Master's)--University of Washington, 2020This work addresses control law synthesis for activ...
This thesis deals with high angle of attack behaviour of a generic delta wing model aircraft. A high...
This dissertation seeks to tackle the aircraft loss-of-control problem by adaptive backup flight con...
In the design of °ight control system modeling uncertainties in the form of param-eter variations is...
This work addresses control law synthesis for active flutter suppression followed by the design and ...
The realm of aircraft flight dynamics analysis reaches from local static stability to global dynamic...
The successful high angle of attack (HAOA) operation of fighter aircraft will necessarily require th...
Current practice for flight control validation relies heavily on linear analyses and nonlinear, high...