[PDF.28yl] Nonlinear H∞ Guidance Design for Missile via Galerkin Approximation

Nonlinear H∞ Guidance Design for Missile via Galerkin Approximation

[PDF.fw41] Nonlinear H∞ Guidance Design for Missile via Galerkin Approximation

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 |  2015-05-18 | Original language:English | PDF # 1 |  9.02 x.24 x5.98l,.35 | File type: PDF | 100 pages

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The consistently developing abilities of adversary's weapon systems have continued to initiate missile guidance design toward enhanced accuracy, high velocity interception and rapid maneuver capabilities. Both theory and extensive simulation studies indicate that classical guidance and optimal guidance methods cannot guarantee the terminal homing accuracy, which is required against a target with unpredictable maneuvers. This is because these two guidance laws operate on ...

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