A Problem Statement on Missile Firing

Venkatamangarao Nampally,S. Ananthi, K. Padmanabhan, Kr Balaji,M. Raghavendra Sharma, Arun Ananthanarayanan, J. Rama

International Journal of Advance Research and Innovative Ideas in Education(2017)

Cited 23|Views3
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Abstract
The control system increasing and is very crucial system in space science. Patriot weapon control computer performs crucial system functions for tracking and intercepting targets, as well as other control tasks. The performance of actuation system plays a decisive role in determining the performance of the flight control system for a highly maneuverable missile. In controlling of l the missile aerodynamics, control surfaces, sometimes called fins, are used. In missile guidance system, to reduce the interception distance, it is important to choose a suitable guidance law and navigation constant. Miss distance as low as 0.012m can be achieved with significantly lower control effort than required by ISM alone.
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Key words
missile firing,problem statement
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