QFT multi-input, multi-output design with non-diagonal, non-square compensation matrices

View on Open Library

QFT multi-input, multi-output design with non-diagonal, non-square compensation matrices

No reviews yet

First published: 1996 1 language

Subjects

Aircraft performance Stability Flight control Matrices (Mathematics) Directional control Robustness (Mathematics) Feedback

Reviews

Log in or sign up to write a review.

No reviews yet. Be the first!

More by R. A. Hess

Assessing aircraft susceptibility to nonlinear aircraft-pilot coupling/pilot-induced oscillations

Assessing aircraft susceptibility to non...

Unified theory for aircraft handling qualities and adverse aircraft--pilot coupling

Unified theory for aircraft handling qua...

You Might Also Like

More in Aircraft performance

Export controls

Export controls

United States. General Accounting Office

Infamous Aircraft

Infamous Aircraft

Robert Jackson

Taxiing, take-off, and landing simulation of the high speed civil transport aircraft

Taxiing, take-off, and landing simulatio...

Mercedes C. Reaves

Low-speed wind-tunnel test of an unpowered high-speed stoppable rotor concept in fixed-wing mode

Low-speed wind-tunnel test of an unpower...

Michael B. Lance

1999 NASA High-Speed Research Program Aerodynamic Performance Workshop

1999 NASA High-Speed Research Program Ae...

NASA High-Speed Research Program Aerodynamic Performance Workshop (1999 Anaheim, Calif.)

Development of advanced methods of structural and trajectory analysis for transport aircraft

Development of advanced methods of struc...

Mark D. Ardema