Flight Dynamics Modeling of Dual-Spin Guided Projectiles

This paper presents a complete nonlinear parameter-dependent mathematical model, as well as a procedure for computing the quasi-linear parameter-varying (q-LPV) model of a class of spin-stabilized canard-controlled guided projectiles. The proposed projectile concept possesses a so-called dual-spin c...

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Veröffentlicht in:	IEEE transactions on aerospace and electronic systems Jg. 53; H. 4; S. 1625 - 1641
Hauptverfasser:	Seve, Florian, Theodoulis, Spilios, Wernert, Philippe, Zasadzinski, Michel, Boutayeb, Mohamed
Format:	Journal Article
Sprache:	Englisch
Veröffentlicht:	New York IEEE 01.08.2017 The Institute of Electrical and Electronics Engineers, Inc. (IEEE) Institute of Electrical and Electronics Engineers
Schlagworte:	Aerodynamic coefficients Aerodynamics Atmospheric modeling Automatic Axes (reference lines) Computational modeling Dynamical systems Engineering Sciences Flight mechanics guided projectiles Mathematical model Nonlinear dynamical systems Nonlinear dynamics Nose Pitch (inclination) Position sensing Projectiles quasi-linear parameter-varying (q-LPV) systems Rolling motion Stability analysis uncertain systems Weapons Yaw guided projectiles uncertain systems Flight mechanics nonlinear dynamical systems quasi-linear parameter-varying (q-LPV) systems
ISSN:	0018-9251, 1557-9603
Online-Zugang:	Volltext
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