Publikationsdatum:
2013-08-31
Beschreibung:
The benefits are demonstrated of a multiobjective optimization based control structure integrated design methodology. An application of the proposed CSI methodology to the integrated design of the Spacecraft COntrol Lab Experiment (SCOLE) configuration is presented. Integrated design resulted in reducing both the control performance measure and the mass. Thus, better overall performance is achieved through integrated design optimization. The mutliobjective optimization approach used provides Pareto optimal solutions by unconstrained minimization of a differentiable KS function. Furthermore, adjusting the parameters gives insight into the trade-offs involved between different objectives.
Schlagwort(e):
SPACECRAFT DESIGN, TESTING AND PERFORMANCE
Materialart:
Fourth NASA Workshop on Computational Control of Flexible Aerospace Systems, Part 1; p 231-25
Format:
application/pdf
