Discrete multiobjective optimization applied to the spacecraft actuators command problem and tested in a hardware-in-the-loop rendezvous simulator
The challenge of commanding efficiently and autonomously spacecraft actuators hasmotivated the investigation of new optimization techniques in order to extend the spacecrafts life and to insure the fulfillment of all mission requirements. The control problem of spacecraft using actuators with confli...
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| Language: | English |
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Instituto Nacional de Pesquisas Espaciais (INPE)
2015
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| Online Access: | http://urlib.net/sid.inpe.br/mtc-m21b/2015/01.30.12.04 |