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Guidance Laws for Boost-Phase Interceptors Launched from UAVs
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Guidance Laws for Boost-Phase Interceptors Launched from UAVs
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Book Chapter
Guidance Laws for Boost-Phase Interceptors Launched from UAVs
2011
Overview
The considered guidance laws were developed without taking into consideration a real missile acceleration ability. The commanded acceleration
is a command to the missile guidance and control system to realize the
prescribed acceleration. However, the missile inability to perform these
commands would demonstrate practical inefciency of the chosen guidance law. That is why the implementation of the guidance laws should be
accompanied with simulation that helps to choose proper guidance law
parameters. Acceleration limits depend on types of interceptors and technology invested in their production. These limits should be taken into consideration on all stages of missile design.
Publisher
CRC Press,Taylor & Francis Group
ISBN
143985095X, 9781439850954
