DocumentCode :
1442045
Title :
Comments on "True proportional navigation with maneuvering target"
Author :
Rao, S.K.
Author_Institution :
Naval Sci. & Tech. Lab., Gov. of India Minist. of Defence, Vigyan Nagar, India
Volume :
33
Issue :
1
fYear :
1997
Firstpage :
273
Lastpage :
274
Abstract :
In the paper by D. Ghose (Jan. 1994), the author rightly pointed about the unrealistic target maneuvers considered by C.D. Yang et al. (1989) and by P.J. Yuan (1992) and he carried out the analysis for the target maneuver which is inversely proportional to the relative velocity component normal to the line of sight (LOs). This target maneuver is somewhat near to a realistic one, but still it suffers from one drawback. With this maneuver, the target pulls a high acceleration when the interceptor is on a collision course and a negligible acceleration when the LOS rate is already high. The author discusses realistic true proportional navigation (RTPN) because conventional true proportional navigation (TPN) is not used in actual scenario. The result is a third-order nonlinear equation.
Keywords :
missile guidance; navigation; nonlinear equations; target tracking; maneuvering target; missiles homing; proportional navigation; third-order nonlinear equation; Acceleration; Aerodynamics; Aerospace and electronic systems; Communication system control; Data communication; Differential equations; Navigation; Nonlinear equations; Sensor fusion; Target tracking;
fLanguage :
English
Journal_Title :
Aerospace and Electronic Systems, IEEE Transactions on
Publisher :
ieee
ISSN :
0018-9251
Type :
jour
DOI :
10.1109/7.570778
Filename :
570778
Link To Document :
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