Unlike the traditional ways adopted by most of the researchers, the rotating angle of relative velocity is adopted in this work as the independent variable to analyze the analytical solution of impact angle, capture region (with or without finite line of sight (LOS) turn rate constraint), range to go, time to go, and a defined fuel cost of a traditional pure proportional navigation (PPN) guidance law for both nonmaneuvering moving, and stationary targets.
Analysis of 3D PPN guidance laws for nonmaneuvering target
IEEE Transactions on Aerospace and Electronic Systems ; 51 , 4 ; 2932-2943
2015-10-01
1274579 byte
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
Impact Angle Constrained Guidance Against Nonstationary Nonmaneuvering Targets
Online Contents | 2010
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