This document describes the design of a flight controller for the Research Civil Aircraft Model (RCAM), suing mu-synthesis. The controller has to satisfy design requirements formulated in a manual prepared by action group FM(AG08) of the GARTEUR organization ((FLi96b)). The resulting control system is implemented in a software environment, in which performance and robustness characteristics are evaluated by simulating a flight along a predefined trajectory.
Design of a Flight Controller for the Research Civil Aircraft Model (RCAM) Using mu-Synthesis
1996
186 pages
Report
Keine Angabe
Englisch
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