The research during the second reporting period has focused on robust control design for hypersonic vehicles. An already existing design for the Hypersonic Winged-Cone Configuration has been enhanced. Uncertainty models for the effects of propulsion system perturbations due to angle of attack variations, structural vibrations, and uncertainty in control effectiveness were developed. Using H(sub infinity) and mu-synthesis techniques, various control designs were performed in order to investigate the impact of these effects on achievable robust performance.
Research in robust control for hypersonic aircraft
1993-10-01
Report
Keine Angabe
Englisch
Research in Robust Control for Hypersonic Aircraft
NTIS | 1993
|Robust control of hypersonic aircraft [6795-189]
British Library Conference Proceedings | 2007
|Robust nonlinear control of a hypersonic aircraft
AIAA | 1999
|Robust Nonlinear Control of a Hypersonic Aircraft
British Library Conference Proceedings | 1999
|Robust Nonlinear Control of a Hypersonic Aircraft
AIAA | 2000
|