DocumentCode :
434003
Title :
Angle constraint biased PNG
Author :
Jeong, S.K. ; Cho, S.J. ; Kim, E.G.
Author_Institution :
Guidance & Control Technol. Div., Agency for Defense Dev., Daejeon, South Korea
Volume :
3
fYear :
2004
fDate :
20-23 July 2004
Firstpage :
1849
Abstract :
In this paper, we propose a new biased proportional navigation guidance (BPNG) to get an arbitrary impact angle against stationary target. The closed form solution of this angle constraint BPNG (named ACBPNG) is derived. And with the solution, we can determine the exact bias for a required impact angle analytically. The solution is shown to be very useful to determine a proper homing guidance condition including initial engaging geometry and missile maneuverability. Because of its handy form to implement and easy solution to analyze, ACBPNG can be the most simple and effective scheme for homing guidance with impact angle constraint. ACBPNG could be applicable to either the system that uses seeker (both active and passive) or the system that does not use seeker.
Keywords :
missile guidance; proportional control; angle constraint biased proportional navigation guidance; homing guidance; initial engaging geometry; missile maneuverability; Acceleration; Closed-form solution; Computer vision; Cost function; Differential equations; Geometry; Leg; Missiles; Navigation; Underwater vehicles;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Control Conference, 2004. 5th Asian
Conference_Location :
Melbourne, Victoria, Australia
Print_ISBN :
0-7803-8873-9
Type :
conf
Filename :
1426914
Link To Document :
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