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A rule based missile evasion method for fighter aircrafts
M Sert - 2008 - search.proquest.com
In this thesis, a new guidance method for fighter aircrafts and a new guidance method for
missiles are developed. Also, guidance and control systems of the aircraft and the missile …
missiles are developed. Also, guidance and control systems of the aircraft and the missile …
Development and comparison of autopilot and guidance algorithms for missiles
Ç Evcimen - 2007 - search.proquest.com
In order to have an interception with a target, a missile should be guided with a successful
guidance algorithm accompanied with a suitable autopilot structure. In this study, different …
guidance algorithm accompanied with a suitable autopilot structure. In this study, different …
A robustness analysis procedure for realistic missiles
RÖ DORUK, E KOCAOĞLAN - Turkish Journal of Electrical …, 2005 - journals.tubitak.gov.tr
This paper presents a robustness analysis procedure for short range realistic missile
autopilots. The sensitivity of the autopilots to the aerodynamic parameter uncertainties is …
autopilots. The sensitivity of the autopilots to the aerodynamic parameter uncertainties is …
A Robustness Analysis Procedure for Realistic Missiles.
R Özgür, E Kocaoğlan - Turkish Journal of Electrical …, 2005 - search.ebscohost.com
This paper presents a robustness analysis procedure for short range realistic missile
autopilots. The sensitivity of the autopilots to the aerodynamic parameter uncertainties is …
autopilots. The sensitivity of the autopilots to the aerodynamic parameter uncertainties is …
[CITATA][C] Projective linear quadratic control of direct current motor under disturbance torques
I Zuglam - 2017 - Fen Bilimleri Enstitüsü