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Recent experience in simultaneous control-structure optimizationTo show the feasibility of simultaneous optimization as design procedure, low order problems were used in conjunction with simple control formulations. The numerical results indicate that simultaneous optimization is not only feasible, but also advantageous. Such advantages come at the expense of introducing complexities beyond those encountered in structure optimization alone, or control optimization alone. Examples include: larger design parameter space, optimization may combine continuous and combinatoric variables, and the combined objective function may be nonconvex. Future extensions to include large order problems, more complex objective functions and constraints, and more sophisticated control formulations will require further research to ensure that the additional complexities do not outweigh the advantages of simultaneous optimization. Some areas requiring more efficient tools than currently available include: multiobjective criteria and nonconvex optimization. Efficient techniques to deal with optimization over combinatoric and continuous variables, and with truncation issues for structure and control parameters of both the model space as well as the design space need to be developed.
Document ID
19900011762
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Salama, M.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Ramaker, R.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Milman, M.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
September 6, 2013
Publication Date
August 1, 1989
Publication Information
Publication: NASA, Langley Research Center, NASA(DOD Controls-Structures Interaction Technology 1989
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
90N21078
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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