DocumentCode
1246286
Title
Solutions of generalized proportional navigation with maneuvering and nonmaneuvering targets
Author
Pin-Jar Yuan ; Shih-Che Hsu
Author_Institution
Chung Shan Inst. of Sci. & Technol., Lung-Tan, Taiwan
Volume
31
Issue
1
fYear
1995
Firstpage
469
Lastpage
474
Abstract
In this generalized proportional navigation (GPN), the commanded acceleration is applied in a direction with a bias angle to the normal direction of line-of-sight (LOS) and its magnitude is proportional to the product of closing speed and LOS rate between interceptor and its target. Some solutions of GPN were obtained before under the assumption that the magnitude of commanded acceleration is proportional to the LOS rate only. Now in this article, the exact and complete closed-form solutions are derived under this modified guidance scheme for both maneuvering and nonmaneuvering targets. Some related important characteristics, such as capture capability and energy cost, are investigated and discussed. The variation of bias angle will induce the change of capture area and energy cost required. Also, a typical example of target maneuver is introduced to describe the effect of target maneuver easily. It shows that the target maneuver will decrease the capture area and increase the energy cost for effective intercept of target.<>
Keywords
missile guidance; navigation; proportional control; target tracking; bias angle; complete closed-form solutions; energy cost; generalized proportional navigation; interceptor; line-of-sight; maneuvering targets; nonmaneuvering targets; normal direction; target maneuver; Acceleration; Closed-form solution; Costs; Differential equations; Energy capture; Geometry; Missiles; Navigation; System performance; Virtual manufacturing;
fLanguage
English
Journal_Title
Aerospace and Electronic Systems, IEEE Transactions on
Publisher
ieee
ISSN
0018-9251
Type
jour
DOI
10.1109/7.366329
Filename
366329
Link To Document