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    Generalized Formulation of Weighted Optimal Guidance Laws with Impact Angle Constraint  
    Chang-Hun Lee(KAIST)
    Korea | IEEE Transactions on Aerospace and Electronic Syst
    2013 | 바로가기
    Acceleration, Cost function, Optimal control, Missiles, Kinematics, Equations
    Cited by 71

    ■ View full text

    IEEE Transactions on Aerospace and Electronic Systems

    https://ieeexplore.ieee.org/abstract/document/6494416

     

     

    ■ Researchers

    Chang-Hun Lee

    Department of Aerospace Engineering, Korea Advanced Institute of Science and Technology (KAIST)

    C. H. Lee*, M. J. Tahk, and J. I. Lee

     

    ■ Abstract

    The generalized formulation of weighted optimal guidance laws with impact angle constraint is investigated here. From the generalized formulation, we explicitly find the feasible set of weighting functions that lead to analytical forms of weighted optimal guidance laws. This result has potential significance because it can provide additional degrees of freedom in designing a guidance law that accomplishes the specified guidance objective.

     

     

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