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).
Design Criteria Multi-Loop Flight Control Systems
1986
12 pages
Report
No indication
English
Avionics , Flight control systems , Flight paths , Aerodynamic control surfaces , Control theory , Nonlinear systems , Aerodynamic characteristics , Open loop systems , Closed loop systems , Integrated systems , West germany , Foreign technology , Component Reports , Flight management systems , Multiloop flight control systems
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