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
197 pages
Report
No indication
English
Aircraft flight test trajectory control
NTRS | 1988
|Aircraft flight test trajectory control
NTRS | 1988
|Aircraft Flight Test Trajectory Control
NTIS | 1988
|