Robust gain-scheduled autopilot design for spin-stabilized projectiles with a course-correction fuze

This article explores the design of a pitch/yaw axis load factor autopilot for a class of 155-mm spin-stabilized ammunition which incorporates a novel nose-positioned course correction fuze system used for trajectory correction. The projectile full nonlinear model is discussed and a procedure for ob...

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Veröffentlicht in:	Aerospace science and technology Jg. 42; S. 477 - 489
Hauptverfasser:	Theodoulis, Spilios, Sève, Florian, Wernert, Philippe
Format:	Journal Article
Sprache:	Englisch
Veröffentlicht:	Elsevier Masson SAS 01.04.2015 Elsevier
Schlagworte:	Actuators Automatic Automatic pilots Autopilot design Design engineering Engineering Sciences Flight mechanics Gain-scheduling Guided projectiles Loads (forces) LPV systems Nonlinearity Projectiles Robust control Stability Trajectories Robust control Autopilot design LPV systems Guided projectiles Gain-scheduling Flight mechanics
ISSN:	1270-9638, 1626-3219
Online-Zugang:	Volltext
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