The MK VI - A second generation attitude control system

Details The MK VI - A second generation attitude control system The MK VI - A second generation attitude control system

Oct 1986

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1986srbr.confr....m&link_type=abstract

AIAA, Conference on Sounding Rockets, Balloons and Related Space Systems, 7th, Ocean City, MD, Oct. 28-30, 1986. 11 p.

Computer Science

Sound

Attitude Control, Halley'S Comet, Microcomputers, Payloads, Sounding Rockets, Spacecraft Maneuvers, Block Diagrams, Pneumatic Control, Pointing Control Systems, Signal To Noise Ratios

Scientific paper

The MK VI, a new multipurpose attitude control system for the exoatmospheric attitude control of sounding rocket payloads, is described. The system employs reprogrammable microcomputer memory for storage of basic control logic and for specific mission event control data. The paper includes descriptions of MK VI specifications and configuration; sensor characteristics; the electronic, analog, and digital sections; the pneumatic system; ground equipment; the system operation; and software. A review of the MK VI performance for the Comet Halley flight is presented. Block diagrams are included.

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