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A theoretical method of analyzing the effects of yaw-damper dynamics on the stability of an aircraft equipped with a second-order yaw damper / by Schy, Albert A.
Published 1952Call Number: Loading…
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A theoretical analysis of the effects of fuel motion on airplane dynamics / by Schy, Albert A.
Published 1951Call Number: Loading…Search for the full-text version of this title in HathiTrust
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3
Pseudosteady-state analysis of nonlinear aircraft maneuvers / by Young, John W. (John Worth), 1934-, Schy, Albert A., Johnson, Katherine G.
Published 1980Call Number: Loading…Online Access
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4
A theoretical method of determining the control gearing and time lag necessary for a specified damping of an aircraft equipped with a constant-time-lag autopilot / by Gates, Ordway B.
Published 1951Other Authors: “…Schy, Albert A.…”
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Pseudosteady-state analysis of nonlinear aircraft maneuvers by Young, John W. (John Worth), 1934-
Published 1980Other Authors: “…Schy, Albert A.…”
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Related Subjects
Airplanes
Control
Aerodynamic characteristics
Aircraft maneuvers
Angle of attack
Automatic control
Automatic pilot (Airplanes)
Damping (Mechanics)
Dynamics
Fighter aircraft
Flight characteristics
Fuel
Fuel tanks
Mathematical analysis
Motion
Pitching (Aerodynamics)
Rolling (Aerodynamics)
Spin (Aerodynamics)
Stability of airplanes
Stability of airplanes, Lateral
Yawing (Aerodynamics)