ANALYTIC DESIGN OF AIRPLANE AUTOMATIC PITCH CONTROLLER

Using given specifications on airplane short-period longitudinal motion, the parameters of an airplane automatic pitch controller of a given structure with angular-pitch-rate and normal-load-factor feedbacks are determined.

  • Corporate Authors:

    Allerton Press, Incorporated

    150 Fifth Avenue
    New York, NY  USA  10011
  • Authors:
    • Sirazetdinov, T K
    • Ivanov, V K
  • Publication Date: 1977

Media Info

  • Features: References;
  • Pagination: p. 53-58
  • Serial:

Subject/Index Terms

Filing Info

  • Accession Number: 00190194
  • Record Type: Publication
  • Source Agency: Engineering Index
  • Files: TRIS
  • Created Date: May 11 1979 12:00AM