NASA NTRS · 19880007324
Aircraft flight test trajectory control
Abstract
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.
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Menon, P. K. A., Walker, R. A.. 1988-01-01. Aircraft flight test trajectory control. https://ntrs.nasa.gov/citations/19880007324
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