An attitude control system for the unmanned hypersonic test vehicle is presented. The key issues of hypersonic vehicle attitude establishment and linear control concept relating to Supersonic Combustion Ramjet test are considered. Robust controller is designed using mixed sensitivity method. The robustness is evaluated by use of CFD data and simulation results developed to date are presented.
Attitude control of unmanned hypersonic test vehicle
2008-12-01
582822 byte
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
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