NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
The application of linear actuators for telescope pointing controlA study team at MSFC has conceptually designed two lunar-based telescopes, a 16 m aperture Large Lunar Telescope (LLT) and a 4 m Cluster Telescope Experiment (CTE). The CTE serves as a technology tested for the LLT. The CTE utilizes a hexapod telescope mount to obtain a small gimbal angle that significantly extends the viewing space and observation time from that of a stationary transit telescope. This paper addresses the applicability of six linear actuators to provide limited gimbal rotation of the CTE telescope assembly. Kinematic constraint equations for the hexapod mount have been applied to a six degree-of-freedom rigid body model. Static equilibrium equations have been solved to address configuration design issues, and a feedback tracking control system has been designed and simulated.
Document ID
19920060662
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Carrington, C. K.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Davis, B. G.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
August 15, 2013
Publication Date
January 1, 1992
Subject Category
Mechanical Engineering
Report/Patent Number
AAS PAPER 91-536
Meeting Information
Meeting: AAS/AIAA Astrodynamics Conference
Location: Durango, CO
Country: United States
Start Date: August 19, 1991
End Date: August 22, 1991
Accession Number
92A43286
Distribution Limits
Public
Copyright
Other

Available Downloads

There are no available downloads for this record.
No Preview Available