The problems of design criteria and architecture of multiloop flight control systems 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 are discussed. Joint root locus and quality criteria design are presented. The structure of the presented multiloop flight control system consists of nonlinear open loop control for flight performance and flight management; superposed quasilinear state vector feedback; and six control surfaces (aileron, rudder, elevator, trim, throttle, direct lift/drag control).
Design Criteria for Multi-Loop Flight Control Systems
1986
12 pages
Report
No indication
English
Avionics , Aerodynamic coefficients , Aerodynamics , Aircraft guidance , Architecture (Computers) , Automatic flight control , Control systems design , Flight management systems , Flight paths , Angle of attack , Block diagrams , Control surfaces , Do-28 aircraft , Flight tests , Fluid flow , Foreign technology
Design Criteria Multi-Loop Flight Control Systems
NTIS | 1986
|Design criteria for optimal flight control systems
AIAA | 1979
|Design Criteria for Optimal Flight Control Systems
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