Computer Science – Sound
Scientific paper
Nov 1991
adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1991esasp.317..237r&link_type=abstract
In ESA, 10th ESA Symposium on European Rocket and Balloon Programmes and Related Research p 237-242 (SEE N92-24589 15-12)
Computer Science
Sound
Attitude Control, Control Systems Design, Data Processing, Inertial Navigation, Inertial Reference Systems, Integrated Circuits, Rocket-Borne Instruments, Sounding Rockets, Systems Integration, Attitude Gyros, Cards, Guidance (Motion), Interfaces, Systems Engineering, Telemetry
Scientific paper
The advantages of integrating guidance, control and telemetry functions into a single unit, and how this was achieved through the development of the MARS TI (Miniature Attitude Reference System TRG (Tuned Rotor Gyros) Instrument) and MARS GC (Guidance Control) rollstable guidance platforms are discussed. The primary advantage of single unit packaging to the sounding rocket and commercial spacecraft user is a significantly lighter and less costly guidance and control overhead. Additional benefits include much more flexibility in the configuration of input and output devices, increased reliability through the reduction of discrete component interfaces, and reduced system weight and power consumption. The development process of both platforms is traced emphasizing the unique application of multifunction integrated circuits to solve packaging versus system capability design trades. Final product configuration flexibility is illustrated through applications examples.
Bailey Richard A.
Rasmussen Richard Eric
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