Compact deformable mirror driver electronics for risk tolerant astrophysics missions
Publisher
SPIECitation
Christian Haughwout, Kyle Van Gorkom, Stephen Kaye, Kerri Cahoy, Daewook Kim, Ewan S. Douglas, "Compact deformable mirror driver electronics for risk tolerant astrophysics missions," Proc. SPIE 12677, Astronomical Optics: Design, Manufacture, and Test of Space and Ground Systems IV, 1267706 (4 October 2023); https://doi.org/10.1117/12.2677714Rights
© 2023 SPIE.Collection Information
This item from the UA Faculty Publications collection is made available by the University of Arizona with support from the University of Arizona Libraries. If you have questions, please contact us at repository@u.library.arizona.edu.Abstract
Deformable mirrors (DMs) are a critical enabling technology for many astrophysics mission concepts currently in development. Unfortunately, generating the control signals required by DMs is difficult, and historically there have been few options for controlling a DM on a spacecraft. In this work, electronics suitable for controlling a 952 actuator MEMS DM have been developed and their performance has been characterized. The driver electronics deliver 16 bits of resolution with a least significant bit increment of 2.75 milliVolts and RMS electronic noise of less than 1.2 milliVolts over the range of 0 to 170 Volts. These electronics have been built to be compatible with the needs of missions that are cost-constrained and risk-tolerant. To that end, the driver electronics use widely available parts with a total expected unit cost of approximately $30,000. Although the driver electronics do not use radiation hardened parts, testing data indicates a 2 year lifetime in a TESS-like orbit with 90 percent confidence when shielded by 6 millimeters of aluminum. © 2023 SPIE.Note
Immediate accessISSN
0277-786XISBN
978-151066568-2Version
Final Published Versionae974a485f413a2113503eed53cd6c53
10.1117/12.2677714