Guidance and Control of Homing Missiles: Dynamic Models of Single- and Two-Part Homing Missiles with Proposed Guidance and Control Schemes - Image 1

£67.63

LAP Lambert Academic Publishing Guidance and Control of Homing Missiles: Dynamic Models of Single- and Two-Part Homing Missiles with Proposed Guidance and Control Schemes

Name: Guidance and Control of Homing Missiles: Dynamic Models of Single- and Two-Part Homing Missiles with Proposed Guidance and Control Schemes
Brand: LAP Lambert Academic Publishing
Price: 67.63 GBP
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Description

Homing missiles have gained wide popularity in the field of guidance and control regarding the short and medium range purposes in recent years. In this study, the three-dimensional formulation of the Proportional Navigation Guidance (PNG) law is done. Another contribution of this study is the derivation of the Linear Homing Guidance (LHG) and the Parabolic Homing Guidance (PHG) laws. Then, all these three methods are implemented on both the considered missile model for the uncanted and canted tail wing configurations, and a generic single-body missile model. Also, the acceleration, rate and angular autopilots are designed in order to realize the guidance commands generated by these guidance laws on the considered missile models. Finally, the overall guidance and control models are constructed by integrating the obtained models and then numerous computer simulations are carried out to test the performance of the system in different scenarios.

Product Specifications

Brand: LAP Lambert Academic Publishing
Format: paperback
ASIN: 3847309617
Category: Books > Subjects > Reference > Transport > Aviation
Domain: Amazon UK
Release Date: 21 December 2011
Listed Since: 24 December 2011

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LAP Lambert Academic Publishing Guidance and Control of Homing Missiles: Dynamic Models of Single- and Two-Part Homing Missiles with Proposed Guidance and Control Schemes

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