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Guidance law to improve the accuracy of tactical missiles
Guidance law to improve the accuracy of tactical missiles
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机译:制导法,以提高战术导弹的准确性
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摘要
A missile guidance system in a canard controlled airframe with means to measure the angle of attack as well as the pursuit angle by the use of a two degree of freedom roll-free reference gyroscope or other inertial reference device so as to move the canard control surfaces, where the canards direct the missile to the target.
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