DocumentCode :
3612957
Title :
Analysis of 3D PPN guidance laws for nonmaneuvering target
Author :
Feng Tyan
Author_Institution :
Dept. of Aerosp. Eng., TamKang Univ., Taipei, Taiwan
Volume :
51
Issue :
4
fYear :
2015
Firstpage :
2932
Lastpage :
2943
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;
fLanguage :
English
Journal_Title :
Aerospace and Electronic Systems, IEEE Transactions on
Publisher :
ieee
ISSN :
0018-9251
Type :
jour
DOI :
10.1109/TAES.2015.140676
Filename :
7376228
Link To Document :
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