H∞ Method Applied to Launcher Control During Atmospheric Flight

Details H∞ Method Applied to Launcher Control During Atmospheric Flight H∞ Method Applied to Launcher Control During Atmospheric Flight

Feb 1997

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1997esasp.381..349m&link_type=gif

Spacecraft Guidance, Navigation and Control Systems, Proceedings of the 3rd ESA International Conference held 26-29 November, 19

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