Robust parametrically varying attitude controller designs for the X-33 vehicle
Open access
Date
2000Type
- Conference Paper
ETH Bibliography
no
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Abstract
Robust linear parameter varying (LPV) control design techniques are applied to the attitude control of the X-33, a single-stage to orbit prototype vehicle. The focus of the research is to develop techniques which will allow for a variety of trajectories without significant redesign of the control system. The LPV design method is described, and applied to a representative problem: control of the pitch axis dynamics during ascent. The work is on-going and this paper details the design problem formulation. Show more
Permanent link
https://doi.org/10.3929/ethz-b-000671602Publication status
publishedExternal links
Book title
AIAA Guidance, Navigation, and Control Conference and ExhibitJournal / series
AIAA Guidance, Navigation and Control Conference and ExhibitPages / Article No.
Publisher
American Institute of Aeronautics and AstronauticsEvent
Subject
attitude control; Single Stage to Orbit; Closed Loop Transfer Function; Aerodynamic Coefficients; Angle of attack; Center of pressure; Quaternions; Marshall Space Flight Center; Thrust vectoring; Flight Control SystemOrganisational unit
08814 - Smith, Roy (Tit.-Prof.)
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ETH Bibliography
no
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