X-33 attitude control using the XRS-2200 linear aerospike engine-Reference-Cited by-同舟云学术

X-33 attitude control using the XRS-2200 linear aerospike engine

Published:1999-06-20 Issue: Volume: Page:
ISSN:
Container-title:35th Joint Propulsion Conference and Exhibit
language:
Short-container-title:

Author:

Hall Charles¹,Panossian Hagop²

Affiliation:

1. NASA, Marshall Space Flight Center, Huntsville, AL

2. Boeing Co., Canoga Park, CA

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1999-2936

Reference7 articles.

1. "Variable StructurePID ControltoPrevent IntegralWindup0022, C.E.Hall,A. S.Hodel,J.Y. Hung,presentationto31"SoutheasternSymposium onSystemTheory,March,21-23,1999

2. "ParametricIdentificationof TransferFunctions in theFrequencyDomain,aSurvey0022,R.Pintelon,P. Guillaume,Y. Rolaine,J.SchoukensandH. Van hamme,Proceedingsof the32"dConferenceon DecisionandControl,SanAntonio, TX.,December, 1993

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