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Dynamics of aerospace vehiclesThe focus of this research was to address the modeling, including model reduction, of flexible aerospace vehicles, with special emphasis on models used in dynamic analysis and/or guidance and control system design. In the modeling, it is critical that the key aspects of the system being modeled be captured in the model. In this work, therefore, aspects of the vehicle dynamics critical to control design were important. In this regard, fundamental contributions were made in the areas of stability robustness analysis techniques, model reduction techniques, and literal approximations for key dynamic characteristics of flexible vehicles. All these areas are related. In the development of a model, approximations are always involved, so control systems designed using these models must be robust against uncertainties in these models.
Document ID
19930009207
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Schmidt, David K.
(Arizona State Univ. Tempe, AZ, United States)
Date Acquired
September 6, 2013
Publication Date
September 1, 1991
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NAS 1.26:192179
NASA-CR-192179
Report Number: NAS 1.26:192179
Report Number: NASA-CR-192179
Accession Number
93N18396
Funding Number(s)
CONTRACT_GRANT: NAG1-1086
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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