Large angle maneuver experiments in ground-based laboratories
Author:
Affiliation:
1. USAF, Astronautics Laboratory, Edwards AFB, CA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1990-1236
Reference31 articles.
1. Avariety of sensors and actuators will be available on the structure. Rapid retargeting torque will be provided using a complement of twelve cold gas thrusters with a peak thrust of 900 N (200 Ibf). The thrusters can be operated either in a bang-bang mode or they can be throttled for shaping the torque profile. A number of reaction wheels and proof mass actuators of sufficient authority will also be available for vibration control. A set of translational and rotational accelerometers will be available for use at various feasible locations throughout the structure. The facility is currently under development and is expected to be operational by the end of 1989.
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1. AIR-JET THRUSTERS EOR ACTIVE VIBRATION CONTROL: DESIGN AND CALIBRATION;Experimental Techniques;1990-11
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