Sounding rocket attitude control utilizing tuned rotor gyros

Details Sounding rocket attitude control utilizing tuned rotor gyros Sounding rocket attitude control utilizing tuned rotor gyros

Jun 1978

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1978esasp.135..449r&link_type=abstract

In ESA European Sounding Rocket, Balloon and Related Res., with Emphasis on Expt. at High Latitudes p 449-456 (SEE N79-31637 2

Computer Science

Sound

Attitude Control, Infrared Instruments, Rotary Gyroscopes, Sounding Rockets, Celestial Bodies, Computer Programming, Digital Systems, Euler Equations Of Motion, Inertial Reference Systems

Scientific paper

A precision Attitude Control System (ACS) for the orientation and scanning of celestial and terrestrial targets with infrared instruments is described. Tuned rotor gyros were selected as the precision inertial references for the ACS. Tuned rotor gyros and their supporting electronics are extensively discussed. The complete mechanization of the ACS is described. Aspects of the digital programmer, digital integration, and important software considerations are highlighted.

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