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An Optimization Approach to Orienting Three Spacecraft Reaction Wheel Actuators with Application to the Europa Orbiter

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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