DocumentCode
2790379
Title
A powerful kinematic model for proportional navigation of guided weapons against maneuvering targets
Author
Shukla, Uday S. ; Mahapatra, Pravas R.
Author_Institution
Dept. of Aerosp. Eng., Indian Inst. of Sci., Bangalore, India
fYear
1989
fDate
22-26 May 1989
Firstpage
194
Abstract
An accurate solution is presented of the nonlinear differential equations describing the pursuer motion under the PN (proportional navigation) law in the general case when the target is laterally maneuvering. A quasilinearization (QL) approach is used, followed by a perturbation technique to obtain analytical solutions to the trajectory parameters. An explicit expression for the pursuer lateral acceleration is derived and is shown to contain contributions due to initial heading error and target maneuver, with a coupling between the two effects. The solution is shown to be a substantial and consistent generalization of the classical linear solution for maneuvering targets. The generalized QL solution presented provides very accurate estimates of pursuer lateral acceleration over a much broader range of engagement geometries and target maneuvers than other presently available analytical solutions
Keywords
navigation; nonlinear differential equations; weapons; analytical solutions; guided weapons; heading error; lateral acceleration; maneuvering targets; nonlinear differential equations; perturbation technique; proportional navigation; pursuer motion; quasilinearization; trajectory parameters; Acceleration; Aircraft navigation; Differential equations; Geometry; Kinematics; Motion analysis; Nonlinear equations; Performance analysis; Perturbation methods; Weapons;
fLanguage
English
Publisher
ieee
Conference_Titel
Aerospace and Electronics Conference, 1989. NAECON 1989., Proceedings of the IEEE 1989 National
Conference_Location
Dayton, OH
Type
conf
DOI
10.1109/NAECON.1989.40212
Filename
40212
Link To Document