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.
Generalized Formulation of Weighted Optimal Guidance Laws with Impact Angle Constraint
IEEE Transactions on Aerospace and Electronic Systems ; 49 , 2 ; 1317-1322
2013-04-01
221993 byte
Article (Journal)
Electronic Resource
English
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