LASER GUIDED MISSILES


abstract

Laser guidance is a technique of guiding a missile or other projectile or vehicle to a target by means of a laser beam. Some laser guided systems utilize beam riding guidance, but most operate more similarly to semi-active radar homing (SARH). This technique is sometimes called SALH, for Semi-Active Laser Homing. With this technique, a laser is kept pointed at the target and the laser radiation bounces off the target and is scattered in all directions (this is known as “painting the target� ....etc

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Definition
Looking back in to the history of rockets and guided missiles, we find that rockets were used in China and India around 1000AD for fire works as well as other purposes. During the 18th Century, unguided rockets propelled missiles were used by 'Hyber Ali' and his son 'Tippu Sulthan' against the British.
The current phase in the history of missiles began during the Second World War with the use of V1 and V2 missiles by the Germany. Since then there has been a rapid growth in this field because of technological development.

Types O ....etc

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what are the advantages and disadvantages???????
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Hiii i m Manjula .I would like to get the notes about past 5years asked ec2050 mobile adhoc network 2 marks with answer ....etc

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i need the ppt of this topic ....etc

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Hi, I am sundar kindly update the question paper of April/may and nov/dec rocket and missiles for regulation 2008. Help me guys. ....etc

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Presented by:Shrenik Mehta
Karan Shah
Jay Pethad
Kunal Kava
Supersonic Cruise Missiles

Introduction:
BrahMos is a supersonic cruise missile that can be launched from submarines, ships, aircraft or land. It is a joint venture between India's Defence Research and Development Organization (DRDO) and Russia's NPO Mashinostroeyenia who have together formed the BrahMos Aerospace Private Limited.
The acronym BrahMos is perceived ....etc

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Guidance Synthesis for Evasive Maneuver of
Anti-Ship Missiles
Against Close-In Weapon Systems
Seminar Report

Presented By
Ms Sarika Raju
st
1 Semester, M.Tech, Roll No:10GNC10

Department of Electrical Engineering
College of Engineering, Trivandrum
Thiruvananthapuram-16
2010
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ae2033 rocket and missiles previous year question paper ....etc

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Abstract
A new suboptimal control method is proposed in this
study to effectively design an integrated guidance and control
system for missiles. Optimal formulations allow designers to
bring together concerns about guidance law performance and
autopilot responses under one unified framework. They lead to
a natural integration of these different functions. By modifying
the appropriate cost functions, different responses, control saturations
(autopilot related), miss distance (guidance related), etc.,
which are of primary concern ....etc

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