Integrated sensor and actuator system for flexible space structure experiments

Details Integrated sensor and actuator system for flexible space structure experiments Integrated sensor and actuator system for flexible space structure experiments

Dec 1985

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1985esasp.231..217l&link_type=abstract

In ESA Second European Space Mechanisms and Tribology Symposium p 217-220 (SEE N86-27353 18-18)

Computer Science

Performance

1

Actuators, Control Systems Design, Flexible Spacecraft, Spacecraft Design, Magnetic Coils, Magnetic Field Configurations, Mechanical Engineering

Scientific paper

A high accuracy sensor and actuator system for laboratory experiments on flexible structure control, comprising an optical sensor and a magnetic actuator, is presented. It features high linearity and large bandwidth. A special wiring profile was realized for the actuator coil to generate a constant magnetic driving field in a defined working space. This design prevents force variations as a result of relative displacement. The performance is confirmed by tests and experiments.

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