Calculation of symmetric response of a jet fighter to atmospheric turbulence and instrument landing system disturbances during approach for landing
By: A. Hyden and Mauritz Sundstrom.
Contributors: Sundstrom, Mauritz.; Royal Institute of Technology (Sweden). Dept. of Aeronautical Engineering
Series: Royal Institute of Technology.  Dept. of Aeronautical Engineering. Technical note -- KTH AERO TN 50
Publisher: Royal Institute of Technology, Dept. of Aeronautical Engineering
Published: 1960
Place of publication: Stockholm
Number of pages: 12
Notes: Bibliographical references: p. 12.