Generalized Formulation of Weighted Optimal Guidance Laws with Impact Angle Constraint

Generalized Formulation of Weighted Optimal Guidance Laws with Impact Angle Constraint

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 sig...

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Veröffentlicht in:IEEE transactions on aerospace and electronic systems 2013-04, Vol.49 (2), p.1317-1322
Hauptverfasser: Lee, Chang-Hun, Tahk, Min-Jea, Lee, Jin-Ik
Format: Artikel
Sprache:eng
Schlagworte:
Acceleration
Aerodynamics
Aircraft components
Cost function
Degrees of freedom
Electronic systems
Equations
Formulations
Impact angle
Kinematics
Laws
Mathematical analysis
Missiles
Optimal control
Optimization
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Zusammenfassung: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.
ISSN:0018-9251
1557-9603
DOI:10.1109/TAES.2013.6494416