Design Criteria Multi-Loop Flight Control Systems

Abstract

The problems of design criteria and architecture of multiloop flight control systems are discussed for a realized system to achieve precise flight path guidance, safe and economic control of the aerodynamic flow (airspeed, angle of attack and lift coefficient control) and passenger comfort. Joint root locus and quality criteria design presented. The structure of the presented multiloop flight control system consists of nonlinear open loop control for flight performance and flight management purpose, superposed quasi linear state vector feed back and six control surfaces (aileron, rudder, elevator, trim, throttle, direct lift/drag control).

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Document Details

Document Type
Technical Report
Publication Date
Dec 01, 1986
Accession Number
ADP005458

Entities

People

  • G. Schsenzer

Organizations

  • AGARD

Tags

Communities of Interest

  • Air Platforms
  • Weapons Technologies

DTIC Thesaurus Topics

  • Air Traffic
  • Air Traffic Control Systems
  • Aircrafts
  • Altitude
  • Control Panels
  • Control Surfaces
  • Control Systems
  • Control Theory
  • Design Criteria
  • Energy
  • Energy Transfer
  • Equations
  • Flight Control Systems
  • Flight Paths
  • Mach Number
  • Measurement
  • Research Aircraft

Fields of Study

  • Physics

Readers

  • Aerodynamics/Aeronautics.
  • Aviation Science / Aeronautics.
  • Control Systems Engineering.

Technology Areas

  • Space
  • Space - Spacecraft Maneuvers