Optimal formation keeping control in missile cooperative engagement

Purpose - The purpose of this paper is to analyze the frame of a missile formation cooperative control system, and present an optimal keeping controller of a missile formation in the cooperative engagement.Design methodology approach - A missile relative motion model is established directly based on...

Celý popis

Uloženo v:

Podrobná bibliografie
Vydáno v:	Aircraft Engineering Ročník 84; číslo 6; s. 376 - 389
Hlavní autoři:	Wei, Changzhu, Shen, Yi, Ma, Xiaoxiao, Guo, Jifeng, Cui, Naigang
Médium:	Journal Article
Jazyk:	angličtina
Vydáno:	Bradford Emerald Group Publishing Limited 01.01.2012
Témata:	Aerospace industry Aircraft Algorithms Control algorithms Control systems Control theory Controllers Design Design engineering Disturbances Frames Kinematics Mathematical models Missiles Optimization Ordinary differential equations Perturbation methods Studies Systems integration Weapons Cooperative engagement Optimal control Control systems Formation flight control Linear quadric optimal Precise integration Programming and algorithm theory
ISSN:	1748-8842, 0002-2667, 1758-4213
On-line přístup:	Získat plný text
Tagy:	Přidat tag Žádné tagy, Buďte první, kdo vytvoří štítek k tomuto záznamu!

Buďte první, kdo okomentuje tento záznam!