نتایج جستجو برای: missile guidance

تعداد نتایج: 79189  

2000
Markus H. Hammer Yuan Zhai Masamichi Katori Thomas Ritter Hans-Dieter Volk Jerzy W. Kupiec-Weglinski

2003
Stephan ten Hagen

— In this paper visual homing is combined with an appearance model to obtain a navigation method that does not require estimates of the pose. The robot's current view is used to select a target from a collection of panoramic images that forms the map. This requires selecting features to find correspondences and in this paper some feature selection methods are evaluated to see which one is best ...

2011
Bruno Jullien

This chapter provides a roadmap to the burgeoning literature on two-sided markets with a speci…c focus on BtoB marketplaces. Online intermediation involves two-sided network e¤ects between buyers and sellers, and the implications for optimal BtoB platforms’tari¤s are discussed. The chapter discusses …rst the monopoly case, drawing attention to the distinction between upfront registration fees a...

In this paper, a new guidance law is designed to improve the performance of a homing missiles guidance system in terminal phase. For this purpose first of all, the two dimensions equations of motion are formulated, then the approximation dynamic of missile control loop is added to these equations which are nonlinear whit unmatched uncertainty. Then, a new adaptive back-stepping method is develo...

1997
Y. Lipman J. Shinar

The interception of a maneuvering antisurface missile, as in ballistic missile defense and ship defense scenarios, is formulated as an imperfect information, zero-sum, pursuit-evasion game with a state constraint imposed on the evader. Assuming that the perfect informationversion of the gamedoes not yield a successful result for the defense, the solution of this game is in mixed strategies. The...

2012
Mustafa Resa Becan Ahmet Kuzucu

A fuzzy predictive pursuit guidance is proposed as an alternative to the conventional methods. The purpose of this scheme is to obtain a stable and fast guidance. The noise effects must be reduced in homing missile guidance to get an accurate control. An aerodynamic missile model is simulated first and a fuzzy predictive pursuit control algorithm is applied to reduce the noise effects. The perf...

Journal: :Int. J. Systems Science 2010
Yu-Ping Lin Lu-Ping Tsao Chun-Liang Lin

This article may be used for research, teaching and private study purposes. Any substantial or systematic reproduction, redistribution , reselling , loan or sub-licensing, systematic supply or distribution in any form to anyone is expressly forbidden. The publisher does not give any warranty express or implied or make any representation that the contents will be complete or accurate or up to da...

Journal: :Journal of Theoretical and Applied Mechanics 2018

Journal: :Journal of the Japan Society for Aeronautical and Space Sciences 1993

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