Flight test of the slide-slope track and flare-control laws for an automatic landing system for a powered-lift STOL airplane /

Flight tests under IFR with an STOL transport aircraft /

Innis, Robert C.
Gallant, Richard P.
Holzhauser, Curt A.
United States. National Aeronautics and Space Administration.
Ames Research Center.

Prepared at Ames Research Center."December 1968"--Cover.Includes bibliographical references (p. 19)....

Crash tests of three identical low-wing single-engine airplanes /

Castle, Claude B.
Alfaro-Bou, Emilio.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1983

Subject category 03."September 1983"--Cover.Distributed to depository libraries in microfiche.Includ...

The landing flare : an analysis and flight-test investigation /

Seckel, Edward, 1921-2009.
Langley Research Center.
Princeton University. Flight Research Laboratory.

"Prepared by Princeton University, [Flight Research Laboratory] ... for Langley Research Center.""Ma...

A flight-test and simulation evaluation of the longitudinal final approach and landing performance of an automatic system for a light wing loading STOL aircraft /

Brown, Stuart C. (Stuart Crockett), 1924-
Hindson, W. S.
Hardy, Gordon H.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1983

Subject category - 08."June 1983."Distributed to depository libraries in microfiche.Includes bibliog...

Flight tests of the Digital Integrated Automatic Landing System (DIALS) /

Halyo, Nesim.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Information & Control Systems, Incorporated.

January 1984

Subject category 08.Distributed to depository libraries in microfiche."December 1984"--Cover."Inform...

Flight-test evaluation of STOL control and flight director concepts in a powered-lift aircraft flying curved decelerating approaches /

Hindson, W. S.
Innis, Robert C.
Hardy, Gordon H.
Ames Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1981

"March 1981"--Cover."Ames Research Center."Includes bibliographical references.Mode of access: Inter...

Design criteria for flightpath and airspeed control for the approach and landing of STOL aircraft /

Franklin, James A.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Ames Research Center.

January 1982

STAR category 08."March 1982"--Cover."Ames Research Center."Includes bibliographical references.Mode...

Development and flight test experiences with a flight-crucial digital control system /

Mackall, Dale A.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Division.

January 1988

"November 1988"--Cover.Includes bibliographical references (p. 52-53).Mode of access: Internet

Experimental investigation of active loads control for aircraft landing gear /

MeGehee, John R.
Dreher, Robert C.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1982

"August 1982"--Cover.Includes bibliographical references.Mode of access: Internet

Development and flight test results of an autothrottle control system at Mach 3 cruise /

Gilyard, Glenn B.
Burken, John J.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.
Hugh L. Dryden Flight Research Center.

January 1980

"July 1980"--Cover.Subject category 08."Dryden Flight Research Center."Mode of access: Internet

Flight test of a pitch control for a spinning vehicle /

Garner, H. Douglas.
Reid, H. J. E.
Langley Research Center.

Prepared at Langley Research Center."July 1963."Cover title.Includes bibliographical references (p. ...

Flight-path and airspeed control during landing approach for powered-lift aircraft /

Franklin, James A.
Innis, Robert C.
Ames Research Center.

January 1974

Prepared at Ames Research Center.Cover title.Includes bibliographical references (p. 59-60).Mode of ...

Aerodynamic and landing measurements obtained during the first powered flight of the North American X-15 research airplane /

United States. National Aeronautics and Space Administration.
Flight Research Center (U.S.)

"January 1960."Cover title.Includes bibliographical references (p. 17).Mode of access: Internet

Flight assessment of a data-link-based navigation-guidance concept /

Abbott, Terrence S.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1983

"April 1983"--Cover.Distributed to depository libraries in microfiche.Mode of access: Internet

Minimum-fuel, three-dimensional flightpath guidance of transport jets /

Neuman, Frank.
Kreindler, E.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1984

Subject category 08."September 1984"--Cover.Distributed to depository libraries in microfiche.Includ...

Flight tests under IFR with an STOL transport aircraft /

Innis, Robert C.
Gallant, Richard P.
Holzhauser, Curt A.
United States. National Aeronautics and Space Administration.
Ames Research Center.

Prepared at Ames Research Center."December 1968"--Cover.Includes bibliographical references (p. 19)....

Crash tests of three identical low-wing single-engine airplanes /

Castle, Claude B.
Alfaro-Bou, Emilio.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1983

Subject category 03."September 1983"--Cover.Distributed to depository libraries in microfiche.Includ...

The landing flare : an analysis and flight-test investigation /

Seckel, Edward, 1921-2009.
Langley Research Center.
Princeton University. Flight Research Laboratory.

"Prepared by Princeton University, [Flight Research Laboratory] ... for Langley Research Center.""Ma...

A flight-test and simulation evaluation of the longitudinal final approach and landing performance of an automatic system for a light wing loading STOL aircraft /

Brown, Stuart C. (Stuart Crockett), 1924-
Hindson, W. S.
Hardy, Gordon H.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1983

Subject category - 08."June 1983."Distributed to depository libraries in microfiche.Includes bibliog...

Flight tests of the Digital Integrated Automatic Landing System (DIALS) /

Halyo, Nesim.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Information & Control Systems, Incorporated.

January 1984

Subject category 08.Distributed to depository libraries in microfiche."December 1984"--Cover."Inform...

Flight-test evaluation of STOL control and flight director concepts in a powered-lift aircraft flying curved decelerating approaches /

Hindson, W. S.
Innis, Robert C.
Hardy, Gordon H.
Ames Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1981

"March 1981"--Cover."Ames Research Center."Includes bibliographical references.Mode of access: Inter...

Design criteria for flightpath and airspeed control for the approach and landing of STOL aircraft /

Franklin, James A.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Ames Research Center.

January 1982

STAR category 08."March 1982"--Cover."Ames Research Center."Includes bibliographical references.Mode...

Development and flight test experiences with a flight-crucial digital control system /

Mackall, Dale A.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Division.

January 1988

"November 1988"--Cover.Includes bibliographical references (p. 52-53).Mode of access: Internet

Experimental investigation of active loads control for aircraft landing gear /

MeGehee, John R.
Dreher, Robert C.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1982

"August 1982"--Cover.Includes bibliographical references.Mode of access: Internet

Development and flight test results of an autothrottle control system at Mach 3 cruise /

Gilyard, Glenn B.
Burken, John J.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.
Hugh L. Dryden Flight Research Center.

January 1980

"July 1980"--Cover.Subject category 08."Dryden Flight Research Center."Mode of access: Internet

Flight test of a pitch control for a spinning vehicle /

Garner, H. Douglas.
Reid, H. J. E.
Langley Research Center.

Prepared at Langley Research Center."July 1963."Cover title.Includes bibliographical references (p. ...

Flight-path and airspeed control during landing approach for powered-lift aircraft /

Franklin, James A.
Innis, Robert C.
Ames Research Center.

January 1974

Prepared at Ames Research Center.Cover title.Includes bibliographical references (p. 59-60).Mode of ...

Aerodynamic and landing measurements obtained during the first powered flight of the North American X-15 research airplane /

United States. National Aeronautics and Space Administration.
Flight Research Center (U.S.)

"January 1960."Cover title.Includes bibliographical references (p. 17).Mode of access: Internet

Flight assessment of a data-link-based navigation-guidance concept /

Abbott, Terrence S.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1983

"April 1983"--Cover.Distributed to depository libraries in microfiche.Mode of access: Internet

Minimum-fuel, three-dimensional flightpath guidance of transport jets /

Neuman, Frank.
Kreindler, E.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1984

Subject category 08."September 1984"--Cover.Distributed to depository libraries in microfiche.Includ...

Flight tests under IFR with an STOL transport aircraft /

Innis, Robert C.
Gallant, Richard P.
Holzhauser, Curt A.
United States. National Aeronautics and Space Administration.
Ames Research Center.

Prepared at Ames Research Center."December 1968"--Cover.Includes bibliographical references (p. 19)....

Crash tests of three identical low-wing single-engine airplanes /

Castle, Claude B.
Alfaro-Bou, Emilio.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1983

Subject category 03."September 1983"--Cover.Distributed to depository libraries in microfiche.Includ...

The landing flare : an analysis and flight-test investigation /

Seckel, Edward, 1921-2009.
Langley Research Center.
Princeton University. Flight Research Laboratory.

"Prepared by Princeton University, [Flight Research Laboratory] ... for Langley Research Center.""Ma...

Flight test of the slide-slope track and flare-control laws for an automatic landing system for a powered-lift STOL airplane /

Abstract

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Flight test of the slide-slope track and flare-control laws for an automatic landing system for a powered-lift STOL airplane /

Abstract

Extracted data

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