AIAA Journal of Guidance Control and Dynamics 1991 Volume 14 Application of multiple input single output analysis procedures to flight test data pdf

AIAA Journal of Guidance Control and Dynamics
1991 Volume 14 Application of multiple input single output analysis procedures to flight test data pdf

Name	AIAA Journal of Guidance, Control, and Dynamics	DOWNLOAD Copy Link Trouble downloading? see How To
Total Size	5.3 GB
Total Files	5675
Hash	D9B94C45954C5EBAE22B251E6993F99C16B7A3A3

/1991 Volume 14/3/Application of multiple-input single-output analysis procedures to flight test data.pdf	1.1 MB
/1992 Volume 15/3/Application of linearization analysis to aircraft dynamics.pdf	655.3 KB
/1993 Volume 16/5/Application of structured singular value synthesis to a fighter aircraft.pdf	1.1 MB
/1996 Volume 19/6/Application of multivariable linear control design to marine towed systems.pdf	923.8 KB
/1996 Volume 19/6/Application of a learning control algorithm to a rotor blade tab.pdf	555.8 KB
/1989 Volume 12/6/Application of output feedback to variable structure systems.pdf	552.2 KB
/1991 Volume 14/6/Application of stochastic robustness to aircraft control systems.pdf	1.2 MB
/1993 Volume 16/1/Application of quantitative feedback theory to a class of missiles.pdf	731.4 KB
/1996 Volume 19/6/Application of real structured singular values to flight control law validation.pdf	1.0 MB
/1993 Volume 16/5/Estimation of Kalman filter gain from output residuals.pdf	686.0 KB
/1994 Volume 17/3/Application of order-n formulation to panel deployment problem of a spacecraft.pdf	415.5 KB
/1995 Volume 18/2/Application of restructurable flight control system to large transport aircraft.pdf	824.5 KB
/1999 Volume 22/2/Application of the Nyquist Stability Criterion on the Nichols Chart.pdf	168.0 KB
/2001 Volume 24/3/Application of Control Structure Design Methods to a Jet Engine.pdf	418.8 KB
/1979 Volume 2/3/Identification of a STOL Propulsion Plant Model from Flight Data.pdf	686.8 KB
Showing first 15 files of 5675 total files