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1 Ergebnisse
1
High angle of attack missile autopilot design by pole place..:
, In:
2010 3rd International Symposium on Systems and Control in Aeronautics and Astronautics
,
Ryu, Sun-Mee
;
Won, Dae-Yeon
;
Lee, Chang-Hun
. - p. 535-539 , 2010
Link:
https://doi.org/10.1109/ISSCAA.2010.5632233
RT T1
2010 3rd International Symposium on Systems and Control in Aeronautics and Astronautics
: T1
High angle of attack missile autopilot design by pole placement approach
UL https://suche.suub.uni-bremen.de/peid=ieee-5632233&Exemplar=1&LAN=DE A1 Ryu, Sun-Mee A1 Won, Dae-Yeon A1 Lee, Chang-Hun A1 Tahk, Min-Jea YR 2010 K1 Missiles K1 Aerodynamics K1 Control systems K1 Gain K1 Mathematical model K1 Damping K1 Time frequency analysis SP 535 OP 539 LK http://dx.doi.org/https://doi.org/10.1109/ISSCAA.2010.5632233 DO https://doi.org/10.1109/ISSCAA.2010.5632233 SF ELIB - SuUB Bremen
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