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Choosing Sensor Configuration for a Flexible Structure Using Full Control SynthesisOptimal locations and types for feedback sensors which meet design constraints and control requirements are difficult to determine. This paper introduces an approach to choosing a sensor configuration based on Full Control synthesis. A globally optimal Full Control compensator is computed for each member of a set of sensor configurations which are feasible for the plant. The sensor configuration associated with the Full Control system achieving the best closed-loop performance is chosen for feedback measurements to an output feedback controller. A flexible structure is used as an example to demonstrate this procedure. Experimental results show sensor configurations chosen to optimize the Full Control performance are effective for output feedback controllers.
Document ID
19980018275
Acquisition Source
Langley Research Center
Document Type
Contractor Report (CR)
Authors
Lind, Rick
(NASA Dryden Flight Research Center Edwards, CA United States)
Nalbantoglu, Volkan
(Minnesota Univ. Minneapolis, MN United States)
Balas, Gary
(Minnesota Univ. Minneapolis, MN United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1997
Subject Category
Aircraft Stability And Control
Report/Patent Number
NAS 1.26:207067
AIAA Paper 97-3745
NASA/CR-97-207067
Report Number: NAS 1.26:207067
Report Number: AIAA Paper 97-3745
Report Number: NASA/CR-97-207067
Meeting Information
Meeting: Guidance, Navigation and Control Conference
Location: New Orleans, LA
Country: United States
Start Date: August 1, 1997
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
CONTRACT_GRANT: N60530-91-C-0218
CONTRACT_GRANT: NSF ECS-91-20354
CONTRACT_GRANT: NAG1-821
CONTRACT_GRANT: JHU-BPO-2229
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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