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Integrated Modeling for the Next Generation Space Telescope "Yardstick" ConceptThe so-called NASA "Yardstick" design concept for the Next Generation Space Telescope presents unique challenges for systems-level analysis. Simulations that integrate controls, optics, thermal, and structural models are required to evaluate baseline performance, study design sensitivities, and perform design optimization. An integrated modeling approach was chosen using a combination of commercial off-the-shelf and "in-house" developed codes. The resulting capability provides a foundation for linear and non-linear analysis, using both the time and frequency-domain methods. It readily allows various combinations of design parameters and environmental loads to be evaluated directly in terms of key science-related metrics, in this case the scalar RMS (root mean square) line-of-sight and RMS wavefront errors. This presentation first addresses the development of the component, or discipline, models for the Yardstick design. It will then proceed to present the integration of the component models, using linear-systems approaches, in order to support two of the most critical baseline performance analyses: jitter and thermal-elastic stability of the optical telescope assembly (OTA). The results of the jitter analysis indicate that disturbances from the reaction wheels coupled with the lightly-damped and highly-flexible structure present significant challenges to the baseline line-of-sight control architecture. Vibration isolation will be required to meet jitter error requirements. The results of the thermal-elastic analysis indicate that the mirror segment displacements due to ground-to-orbit cool-down of the telescope are within the expected capture range of the segment rigid-body control actuators. This means we will be able to align and phase the primary mirror. However, the results for the analysis of the thermal transient response following an attitude maneuver (slew) show that this telescope design is not sufficiently stable, passively, to meet the wavefront error requirements. Structural re-design is one possibility; alternatively, active thermal control of the OTA may be considered. The Yardstick integrated models were successfully used to demonstrate the feasibility of two thermal control strategies.
Document ID
20010089365
Acquisition Source
Goddard Space Flight Center
Document Type
Conference Paper
Authors
Mosier, Gary E.
(NASA Goddard Space Flight Center Greenbelt, MD United States)
Broduer, Steve
Date Acquired
August 20, 2013
Publication Date
January 14, 2001
Subject Category
Astronomy
Meeting Information
Meeting: FEMCI Workshop 2001: Innovative FEM Solutions to Challenging Problems
Location: Greenbelt, MD
Country: United States
Start Date: May 16, 2001
End Date: May 17, 2001
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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