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An Optimization Approach to Orienting Three Spacecraft Reaction Wheel Actuators with Application to the Europa Orbiter
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An Optimization Approach to Orienting Three Spacecraft Reaction Wheel Actuators with Application to the Europa Orbiter
Bayard, D.
URI:
http://hdl.handle.net/2014/16057
Date:
2000
Citation:
n/a
USA
Abstract:
This report introduces an optimization approach to finding the best way to orient three reaction wheels on an orbiting spacecraft.
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JPL TRS 1992+
JPL TRS 1992+
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