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1
Time-optimal attitude control scheme for a spinning missile:
Jahangir, E.
;
Howe, R. M.
Journal of Guidance, Control, and Dynamics. 16 (1993) 2 - p. 346-353 , 1993
Link:
https://doi.org/10.2514/3.21009
RT Journal T1 <Title>Time-optimal attitude control scheme for a spinning missile</Title> UL https://suche.suub.uni-bremen.de/peid=cr-10.2514_3.21009&Exemplar=1&LAN=DE A1 Jahangir, E. A1 Howe, R. M. PB American Institute of Aeronautics and Astronautics (AIAA) YR 1993 SN 0731-5090 SN 1533-3884 JF Journal of Guidance, Control, and Dynamics VO 16 IS 2 SP 346 OP 353 LK http://dx.doi.org/https://doi.org/10.2514/3.21009 DO https://doi.org/10.2514/3.21009 SF ELIB - SuUB Bremen
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