An Entry Range Correction Scheme for Reusable Launch Vehicle

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Abstract:

An entry range correction scheme for reusable launch vehicle (RLV) is developed to reduce the deviation between the predicted range and the computed range. Firstly the physical mechanism is turned out to verify the scheme , then implementation is demonstrated. At last, simulation results illustrate this scheme is able to reduce the deviation, and this scheme is practicality useful.

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406-411

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October 2014

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© 2014 Trans Tech Publications Ltd. All Rights Reserved

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