A flight determination of the attitude control power and damping requirements for a visual hovering task in variable stability and control X-14A research vehicle

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086 0 ‡aNAS 1.14:D-1328
088 ‡aNASA-TN-D-1328
100 0 ‡aRolls, L. Stewart.
245 1 2 ‡aA flight determination of the attitude control power and damping requirements for a visual hovering task in variable stability and control X-14A research vehicle / ‡cby L. Stewart Rolls and Fred J. Drinkwater III.
260 ‡aWashington, D.C. : ‡bNational Aeronautics and Space Administration : ‡b[For sale by the Office of Technical Services, Dept. of Commerce], ‡c[1962]
300 ‡a20 p. : ‡bill. ; ‡c26 cm.
490 0 ‡aNASA technical note ; ‡vNASA TN D-1328
500 ‡aCover title.
500 ‡a"May 1962."
500 ‡aAerodynamics, aircraft; Aircraft; Aircraft safety and noise; Piloting; Simulators and computers; Stability and control.
504 ‡aIncludes bibliographical references.
538 ‡aMode of access: Internet.
650 7 ‡aStability and control. ‡2nasat
650 7 ‡aSimulators and computers. ‡2nasat
650 7 ‡aPiloting. ‡2nasat
650 7 ‡aAircraft safety and noise. ‡2nasat
650 7 ‡aAircraft. ‡2nasat
650 7 ‡aAerodynamics, aircraft. ‡2nasat
700 0 ‡aDrinkwater, Fred J.
710 2 ‡aUnited States. ‡bNational Aeronautics and Space Administration.
CID ‡a011442387
DAT 0 ‡a20101105093916.0 ‡b20141009010000.0
DAT 1 ‡a20141112165512.0 ‡b2023-03-14T18:21:49Z
CAT ‡aSDR-UIUC ‡dUNKNOWN ‡lloader.pl-003-020
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