Computer Science – Sound
Scientific paper
Aug 2003
adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=2003esasp.530..147l&link_type=abstract
In: 16th ESA Symposium on European Rocket and Balloon Programmes and Related Research, 2 - 5 June 2003, Sankt Gallen, Switzerlan
Computer Science
Sound
Space Flight: Techniques, Instrumentation, Ranges
Scientific paper
Saab Ericsson Space has continued its development of digital control systems, based on its previous experiences from the Maxus GCS and DS19. Two new systems now exist: The S19D guidance and control system, which uses DS19 hardware to execute S19 type guidance and control. The GCS/DMARS guidance, navigation and control system, which is a modernisation of the GCS/RIINS. The family of guidance systems provided by Saab Ericsson Space now includes: The analog S19 and the digital S19D for constant attitude guidance during the first part of a sounding rocket's powered flight. The DS19, that controls the attitude throughout the motor burn phase and navigates the vehicle to a pre-set impact point. The (Maxus) GCS with the same function as the DS19, but using thrust vector control via moveable nozzles instead of canard control. The SPINRAC and the RACS, providing exo-atmospheric impact point and attitude control by on-board thrusters.
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