AIAA Journal of Guidance Control and Dynamics 1998 Volume 21 Development and Flight Testing of Parameter Identification Algorithm for Reconfigurable Control pdf

AIAA Journal of Guidance Control and Dynamics
1998 Volume 21 Development and Flight Testing of Parameter Identification Algorithm for Reconfigurable Control 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

/1998 Volume 21/6/Development and Flight Testing of a Parameter Identification Algorithm for Reconfigurable Control.pdf	323.2 KB
/1996 Volume 19/4/Development and flight test of terrain-referenced guidance with ladar forward sensor.pdf	1.2 MB
/1980 Volume 3/2/Implicit Model Following and Parameter Identification of Unstable Aircraft.pdf	571.9 KB
/1978 Volume 1/4/Nonlinear Method for Parameter Identification Applied to a Trajectory Estimation Problem.pdf	364.7 KB
/1985 Volume 8/2/Design and flight testing of digital direct side-force control laws.pdf	1.4 MB
/2006 Volume 29/2/Design and Flight Testing of an H00 Controller for a Robotic Helicopter.pdf	2.0 MB
/1983 Volume 6/3/Development and test of an integrated sensory system for advanced aircraft.pdf	785.6 KB
/1984 Volume 7/3/Design and flight test of a lateral-directional command augmentationsystem.pdf	989.9 KB
/1989 Volume 12/4/Single-mode projection filters for modal parameter identification for flexible structures.pdf	1.0 MB
/1990 Volume 13/1/Spacecraft mass property identification with torque-generating control.pdf	548.1 KB
/1995 Volume 18/3/System identification for adaptive and reconfigurable control.pdf	1.0 MB
/1996 Volume 19/6/Global-local observer Markov parameter identification for system realization.pdf	766.3 KB
/1980 Volume 3/4/Development of an Active Flutter Margin Augmentation System for a Commerical Transport.pdf	1.2 MB
/1987 Volume 10/2/Development and application of a convolution technique for flying qualities research.pdf	1.1 MB
/1988 Volume 11/3/Application of parameter estimation to highly unstable aircraft.pdf	904.7 KB
Showing first 15 files of 5675 total files