The purpose of this paper is to present the results of a design effort to improve F-14 carrier landing performance by the incorporation of the Direct Lift Control into the aircraft's control system. This was done using a new design methodology whereby typical SISO design specifications were translated into the weighting functions of an H(sub infinity), output-feedback synthesis problem. Finally, a technique is presented for the simplification of the Structured uncertainty model for the air vehicles.
Design of an AutoLand Controller for a Carrier-Based F-14 Aircraft Using H infinity Output-Feedback Synthesis
1994
6 pages
Report
Keine Angabe
Englisch
Design of an Autoland Controller for an F-14 Aircraft Using H(infinity) Synthesis
Online Contents | 1996
|Engineering Index Backfile | 1967
NTRS | 1982
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