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- W2364113360 abstract "Scout missile has the characteristic of constant height and constant velocity cruise-flying,so the whole flight track can be divided into beeline-stage and wheeling stage.Under the reasonable hypothesis,a guidance approach can be brought forward: using position control method and deviation angle control method in the beeline-stage and using the swerve control method in the wheeling-stage in order to complete the guidance of whole track and insure that in the flying of scout missile the error of deviating from flight track is relatively small." @default.
- W2364113360 created "2016-06-24" @default.
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- W2364113360 date "2010-01-01" @default.
- W2364113360 modified "2023-09-23" @default.
- W2364113360 title "Guidance Approach Study for Scout Missile Flight Track" @default.
- W2364113360 hasPublicationYear "2010" @default.
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