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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Vydané v:	Aerospace science and technology Ročník 42; s. 477 - 489
Hlavní autori:	Theodoulis, Spilios, Sève, Florian, Wernert, Philippe
Médium:	Journal Article
Jazyk:	English
Vydavateľské údaje:	Elsevier Masson SAS 01.04.2015 Elsevier
Predmet:	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
On-line prístup:	Získať plný text
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