Paper
10 August 2010 An attitude control testbed for JDEM
Kevin Reil, Aaron Roodman, Mike Sholl
Author Affiliations +
Abstract
A mission critical goal of the JDEM mission is to resolve distant galaxies both optically and spectroscopically. In order to achieve this goal, the spacecraft must make observations at the diffraction limit. A full scale attitude control testbed was developed to determine the ability of preliminary designs to meet stringent attitude control requirements. We demonstrate our ability to control a realistic spacecraft structure to ~20 mas. Expected reaction wheel feedback effects are observed and mitigation discussed.
© (2010) COPYRIGHT Society of Photo-Optical Instrumentation Engineers (SPIE). Downloading of the abstract is permitted for personal use only.
Kevin Reil, Aaron Roodman, and Mike Sholl "An attitude control testbed for JDEM", Proc. SPIE 7731, Space Telescopes and Instrumentation 2010: Optical, Infrared, and Millimeter Wave, 77313G (10 August 2010); https://doi.org/10.1117/12.857430
Advertisement
Advertisement
RIGHTS & PERMISSIONS
Get copyright permission  Get copyright permission on Copyright Marketplace
KEYWORDS
Space operations

Sensors

Mirrors

Computing systems

Calibration

Control systems

Observatories

RELATED CONTENT

The JWST science instrument payload: mission context and status
Proceedings of SPIE (September 26 2013)
Arcus: the x-ray grating spectrometer explorer
Proceedings of SPIE (September 30 2016)
JWST cryo fine guidance closed loop test results
Proceedings of SPIE (July 12 2018)
Overview of the James Webb Space Telescope (JWST) project
Proceedings of SPIE (August 18 2005)
On orbit science in a small package managing the...
Proceedings of SPIE (September 23 1994)
Design for an 8-meter monolithic UV/OIR space telescope
Proceedings of SPIE (August 26 2009)

Back to Top