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Optimal Flapping-Wing Vehicle Dynamics via Floquet Multipli..:
Stanford, Bret
;
Beran, Philip
;
Patil, Mayuresh
Journal of Guidance, Control, and Dynamics. 36 (2013) 2 - p. 454-466 , 2013
Link:
https://doi.org/10.2514/1.57213
RT Journal T1 <Title>Optimal Flapping-Wing Vehicle Dynamics via Floquet Multiplier Sensitivities</Title> UL https://suche.suub.uni-bremen.de/peid=cr-10.2514_1.57213&Exemplar=1&LAN=DE A1 Stanford, Bret A1 Beran, Philip A1 Patil, Mayuresh PB American Institute of Aeronautics and Astronautics (AIAA) YR 2013 SN 0731-5090 SN 1533-3884 JF Journal of Guidance, Control, and Dynamics VO 36 IS 2 SP 454 OP 466 LK http://dx.doi.org/https://doi.org/10.2514/1.57213 DO https://doi.org/10.2514/1.57213 SF ELIB - SuUB Bremen
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