Title :
Analysis of 3D PPN guidance laws for nonmaneuvering target
Author_Institution :
Dept. of Aerosp. Eng., TamKang Univ., Taipei, Taiwan
Abstract :
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.
Keywords :
marine navigation; missile guidance; 3D PPN guidance law analysis; LOS turn rate constraint; line of sight turn rate constraint; nonmaneuvering target; pure proportional navigation; Acceleration; Aerodynamics; Angular velocity; Cities and towns; Missiles; Navigation; Three-dimensional displays;
Journal_Title :
Aerospace and Electronic Systems, IEEE Transactions on
DOI :
10.1109/TAES.2015.140676
