Accession Number:

ADA000128

Title:

VTOL Airplane Control in Transition Regimes,

Descriptive Note:

Corporate Author:

FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Personal Author(s):

Report Date:

1974-10-07

Pagination or Media Count:

22.0

Abstract:

The paper examines, from the problem formulation aspect, a fundamental scheme for semiautomatic control of the airplane in the transition regimes, which provides both reliable control of the airplane by the pilot and automatic stabilization of the airplane relative to the center of gravity.

Subject Categories:

  • Aerodynamics
  • VSTOL

Distribution Statement:

APPROVED FOR PUBLIC RELEASE