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Stability boundaries for command augmentation systemsThe Stability Augmentation System (SAS) is a special case of the Command Augmentation System (CAS). Control saturation imposes bounds on achievable commands. The state equilibrium depends only on the open loop dynamics and control deflection. The control magnitude to achieve a desired command equilibrium is independent of the feedback gain. A feedback controller provides the desired response, maintains the system equilibrium under disturbances, but it does not affect the equilibrium values of states and control. The saturation boundaries change with commands, but the location of the equilibrium points in the saturated region remains unchanged. Nonzero command vectors yield saturation boundaries that are asymmetric with respect to the state equilibrium. Except for the saddle point case with MCE control law, the stability boundaries change with commands. For the cases of saddle point and unstable nodes, the region of stability decreases with increasing command magnitudes.
Document ID
19870013189
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Shrivastava, P. C.
(Princeton Univ. NJ, United States)
Date Acquired
September 5, 2013
Publication Date
May 1, 1987
Publication Information
Publication: NASA. Langley Research Center Joint University Program for Air Transportation Research, 1984
Subject Category
Aircraft Stability And Control
Accession Number
87N22622
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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