DocumentCode
1882260
Title
Hysteresis modeling and go-to control of deformable mirrors in adaptive optics
Author
Vogel, Curtis R.
Author_Institution
Opt. Sci. Co., Anaheim, CA, USA
fYear
2012
fDate
3-10 March 2012
Firstpage
1
Lastpage
5
Abstract
We propose a model-based approach to provide “open-loop” control, or precise go-to capability, for piezo actuated deformable mirrors (DMs) used in adaptive optics. Our DM model consists of a two-dimensional, linear partial differential equation known as the thin plate equation to describe the DM facesheet which is coupled to nonlinear scalar ordinary differential equations to describe the hysteretic actuators. Our control approach is carried out in two stages. In the first stage we compute actuator loads that drive the DM facesheet to a prescribed shape. The second stage involves the solution of “inverse” ordinary differential equations that provide the command voltages that induce actuator loads computed in the first stage. This work is significant in that it may enhance predictive and feed-forward control schemes in adaptive optics. Standard integral controllers, operating in closed loop, may also benefit since the gain may be increased.
Keywords
adaptive optics; closed loop systems; hysteresis; mirrors; nonlinear differential equations; open loop systems; optical control; partial differential equations; piezoelectric actuators; DM facesheet; actuator loads; adaptive optics; closed loop control; feed-forward control; go-to capability; go-to control; hysteresis modeling; hysteretic actuators; integral controllers; inverse ordinary differential equations; model-based approach; nonlinear scalar ordinary differential equations; open-loop control; piezoactuated deformable mirrors; thin plate equation; two-dimensional linear partial differential equation; Actuators; Adaptation models; Delta modulation; Hysteresis; Load modeling; Mathematical model; Mirrors;
fLanguage
English
Publisher
ieee
Conference_Titel
Aerospace Conference, 2012 IEEE
Conference_Location
Big Sky, MT
ISSN
1095-323X
Print_ISBN
978-1-4577-0556-4
Type
conf
DOI
10.1109/AERO.2012.6187161
Filename
6187161
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