Two control law design techniques are compared and the performance of the resulting controllers evaluated. The design requirement is for a flight test trajectory controller (FTTC) capable of closed-loop, outer-loop control of an F-15 aircraft performing high-quality research flight test maneuvers. The maneuver modeling, linearization, and design methodologies utilized in this research, are detailed. The results of applying these FTTCs to a nonlinear F-15 simulation are presented.
Aircraft Flight Test Trajectory Control
1988
198 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
|