NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login

Press Enter or click the Search button to begin your search.

Back to Results
Design of a model following, state variable feedback controller for the X-14 VTOL aircraftA model-following, state variable feedback controller is designed for the roll axis of the X-14. The approach is to define a criterion on roll axis performance and to find the gradient of this criterion in the space of parameters (the feedback gains) of the controller. The gradient is then used in a conjungate gradient descent sequence to numerically optimize the parameters.
Document ID
19950028569
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Hasdorff, L. (Virginia Polytechnic Inst. and State Univ. Blacksburg, VA, United States)
Corliss, L. D. (Army Air Mobility Research and Development, Moffett Field, CA United States)
Gossett, T. D. (Army Air Mobility Research and Development, Moffett Field, CA United States)
Date Acquired
August 16, 2013
Publication Date
November 20, 1970
Publication Information
Publisher: Univ. of Santa Clara
Subject Category
Aircraft Stability And Control
Accession Number
95A60168
Distribution Limits
Public
Copyright
Other

Available Downloads

There are no available downloads for this record.

Related Records

There are no records associated with this record.
No Preview Available