Two design techniques for linear flight test trajectory controllers (FTTCs) are described: Eigenstructure assignment and the minimum error excitation technique. The two techniques are used to design FTTCs for an F-15 aircraft model for eight different maneuvers at thirty different flight conditions. An evaluation of the FTTCs is presented.
Aircraft flight test trajectory control
1988-01-01
Report
Keine Angabe
Englisch
Aircraft Flight Test Trajectory Control
NTIS | 1988
|Aircraft flight test trajectory control
NTRS | 1988
|Aircraft Flight Test Trajectory Control
NTIS | 1988
|