An optimal midcourse guidance method for dual pulse air-to-air missiles using linear Gauss pseudospectral model predictive control method
Chinese Journal of Aeronautics
Chinese Journal of Aeronautics ; 38 , 2 ; 103199
01.02.2025
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
Near-optimal midcourse guidance for air-to-air missiles
AIAA | 1990
|Design of Optimal Midcourse Guidance Sliding-Mode Control for Missiles with TVC
Online Contents | 2003
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