Feedback control for flexible landing approach profiles of rotary wing aircraft was investigated. The feedback control circuit, in which the state vector contains 8 variables, is described. Solutions to the linearized state equation are illustrated by examples with results of simulation, during which straight-line, curved, and spatially curved approaches were investigated.
Control Technique in Steep Approach of Rotary Wing Aircraft Regelungstechnik bei Steilanfluegen von Drehflueglern
1973
26 pages
Report
Keine Angabe
Englisch
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