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 :
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