2008
DOI: 10.1109/aero.2008.4526541
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Direct Drive Precision Linear Actuator for Space Interferometry Mission (SIM) Siderostat Pointing

Abstract: SIM PlanetQuest will exploit the classical measuring tool of astrometry (interferometry) with unprecedented precision to make dramatic advances in many areas of astronomy and astrophysics." (1) In order to achieve the required pointing precision of SIM, a gimbaled Siderostat (SID) pointing mechanism with coarse and fine stage actuators is being employed. In order to better understand the coarse pointing accuracy, a team of engineers set out to design, build, and test a linear ballscrew actuator that can perfor… Show more

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Cited by 6 publications
(5 citation statements)
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“…Additionally, for a given length, L, the flexure properties affect the output properties including the energy transfer efficiency, R E , which is defined by Eq. (12). Greater R E yields higher output force for the same maximum displacement.…”
Section: Piezoelectric Actuator Sma Wiresmentioning
confidence: 93%
See 3 more Smart Citations
“…Additionally, for a given length, L, the flexure properties affect the output properties including the energy transfer efficiency, R E , which is defined by Eq. (12). Greater R E yields higher output force for the same maximum displacement.…”
Section: Piezoelectric Actuator Sma Wiresmentioning
confidence: 93%
“…In Eq. (12), ‫ܧ‬ is the maximum output energy from the piezoelectric stack with the ideally preloaded mechanism which is the integral over both the push and pull actuation. ‫ܧ‬ ௨௧ is the maximum output energy from the buckling actuator which is the integral over both the push and pull actuation from the maximum actuation of the piezoelectric stack.…”
Section: Piezoelectric Actuator Sma Wiresmentioning
confidence: 99%
See 2 more Smart Citations
“…7 Linear actuators were used as a variable length linkages to incite rotation about each degree of freedom. [8][9][10] The ARTEMIS control system uses a simplified approach to control the pointing of the telescope when compared to other inertially stabilized systems that are commonly implemented for target tracking. 11 The simplified system treats both the azimuth and elevation axes as completely independent degrees of freedom and implements two distinct single input single output controllers for both axes.…”
Section: Introductionmentioning
confidence: 99%