FLIGHT TEST OF STICK FORCE STABILITY IN ATTITUDE-STABILIZED AIRCRAFT

The investigation described in this paper was aimed at the establishment of a possible need for a criterion of the level of artificial stick force stability during the landing approach of pitch attitude stabilized jet transport aircraft.

  • Availability:
  • Corporate Authors:

    American Institute of Aeronautics and Astronautics

    1290 Avenue of the Americas
    New York, NY  USA  10019
  • Authors:
    • Mooij, H A
    • Gool, MFC van
  • Publication Date: 1978-9

Media Info

  • Features: References;
  • Pagination: p. 562-566
  • Serial:
    • Journal of Aircraft
    • Volume: 15
    • Issue Number: 9
    • Publisher: American Institute of Aeronautics and Astronautics
    • ISSN: 0021-8669

Subject/Index Terms

Filing Info

  • Accession Number: 00188615
  • Record Type: Publication
  • Source Agency: Engineering Index
  • Files: TRIS
  • Created Date: Mar 14 1979 12:00AM