DocumentCode
2386001
Title
Closed-form solution of Pure Proportional Navigation with tracker-in-loop
Author
Garai, Tanushree ; Mukhopadhyay, Siddhartha
Author_Institution
Dept. of Electr. Eng., Indian Inst. of Technol., Kharagpur
fYear
2008
fDate
11-13 June 2008
Firstpage
2352
Lastpage
2357
Abstract
The analytical closed form solution of the equations of motion of a missile tracking a non-maneuvering target using the pure proportional navigation (PPN) law based on an estimate of line-of-sight (LOS) rate is presented. The solution is obtained in the form of a uniformly convergent series of functions in polar coordinates for navigation constants Nges2. The effect of error bounds of the estimator on the closed loop solution is presented, in line with the approach of Becker [1].
Keywords
Kalman filters; differential equations; missiles; navigation; target tracking; closed-form solution; line-of-sight rate; missile tracking; motion equations; navigation constants; nonmaneuvering target; polar coordinates; pure proportional navigation; tracker-in-loop; Acceleration; Closed-form solution; Computational geometry; Equations; Filters; Kinematics; Missiles; Motion control; Navigation; Target tracking; Closed-form solution; Estimator; Guidance; PPN;
fLanguage
English
Publisher
ieee
Conference_Titel
American Control Conference, 2008
Conference_Location
Seattle, WA
ISSN
0743-1619
Print_ISBN
978-1-4244-2078-0
Electronic_ISBN
0743-1619
Type
conf
DOI
10.1109/ACC.2008.4586843
Filename
4586843
Link To Document