CUED Publications database

Design and development of a wind tunnel model for high angle of attack active control experiments

Papageorgiou, G and Glover, K (1997) Design and development of a wind tunnel model for high angle of attack active control experiments. In: UNSPECIFIED pp. 1370-1375..

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Abstract

Aircraft that are able to fly at high angles of attack are very maneuverable. There are a number of interesting control problems associated with fighters performing PST maneuvers. A wind tunnel model was built to help develop and evaluate control law design methods. The rig design is described in some detail. Some open loop features of the model that restrict the achievable closed loop performance are presented. The use of H∞loop-shaping to design controllers for the rig is motivated. A preliminary controller design is presented and tested in simulation.

Item Type: Conference or Workshop Item (UNSPECIFIED)
Subjects: UNSPECIFIED
Divisions: Div F > Control
Depositing User: Cron Job
Date Deposited: 17 Jul 2017 19:37
Last Modified: 24 Oct 2019 14:14
DOI: