Application of the concept of dynamic trim control to automatic landing of Carrier aircraft

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050 ⊔ 4 ‡aTL521.3 ‡b.N18 no. 1512
074 ⊔ ⊔ ‡a830-H-15 (microfiche)
086 0 ⊔ ‡aNAS 1.60:1512
100 1 ⊔ ‡aSmith, Allan G.
245 1 0 ‡aApplication of the concept of dynamic trim control to automatic landing of Carrier aircraft / ‡cAllan Smith and George Meyer.
260 ⊔ ⊔ ‡aWashington, D.C. : ‡bNational Aeronautics and Space Administration, Scientific and Technical Information Office ; ‡a[Springfield, Va. : ‡bFor sale by the National Technical Information Service], ‡c1980.
300 ⊔ ⊔ ‡a82 p. : ‡bill. ; ‡c27 cm.
490 ⊔ 0 ‡aNASA technial paper ; ‡v1512
500 ⊔ ⊔ ‡a"Ames Research Center."
500 ⊔ ⊔ ‡a"April 1980"--Cover.
504 ⊔ ⊔ ‡aIncludes bibliographical references.
538 ⊔ ⊔ ‡aMode of access: Internet.
650 ⊔ 0 ‡aAirplanes ‡xLanding ‡xExperiments.
650 ⊔ 0 ‡aAirplanes ‡xControl systems ‡xExperiments.
650 ⊔ 0 ‡aAirplanes, Military.
700 1 ⊔ ‡aMeyer, George.
710 2 ⊔ ‡aAmes Research Center.
710 1 ⊔ ‡aUnited States. ‡bNational Aeronautics and Space Administration. ‡bScientific and Technical Information Office.
CID ⊔ ⊔ ‡a011423959
DAT 0 ⊔ ‡a20100930161431.0 ‡b20141013010000.0
DAT 1 ⊔ ‡a20141112173021.0 ‡b2025-01-02T19:02:45Z
DAT 2 ⊔ ‡a2025-01-02T18:30:02Z
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