Generalized Formulation of Weighted Optimal Guidance Laws with Impact Angle Constraint
arXiv:1209.1154 · doi:10.1109/TAES.2013.6494416
Abstract
The purpose of this paper is to investigate the generalized formulation of weighted optimal guidance laws with impact angle constraint. 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.
This work has been accepted for publication in IEEE Transactions on Aerospace and Electronic Systems (in press)