Title :
Analytical solution of 3D true proportional navigation
Author :
Ciann-Dong Yang ; Chi-Ching Yang
Author_Institution :
Inst. of Aeronaut. & Astronaut., Nat. Cheng Kung Univ., Tainan
fDate :
10/1/1996 12:00:00 AM
Abstract :
The commanded acceleration applying in the direction normal to the line of sight (LOS) between the interceptor and its target is called true proportional navigation (TPN). The main goal of this work is to derive the complete analytical solutions of three-dimensional (3D) TPN for nonmaneuvering and maneuvering targets. Three coupled nonlinear second-order state equations describing the relative motion are solved analytically without any linearization for performance and trajectory analysis. Properties of 3D TPN such as capture region, range-to-go, time-to-go, and two aspect angles within spherical coordinates are all obtained in closed form. Furthermore, the comparison between 3D TPN and 3D realistic true proportional navigation (RTPN) is investigated analytically in the two-player game where a TPN-guided missile is commanded to pursue a RTPN-guided target, and vice versa
Keywords :
game theory; military systems; missile guidance; nonlinear equations; target tracking; 3D true proportional navigation; TPN; aspect angles; capture region; coupled nonlinear second-order state equations; maneuvering targets; nonmaneuvering targets; range-to-go; spherical coordinates; time-to-go; trajectory analysis; two-player game; Acceleration; Accelerometers; Couplings; Differential equations; Missiles; Motion analysis; Navigation; Nonlinear equations; Performance analysis; Rotation measurement;
Journal_Title :
Aerospace and Electronic Systems, IEEE Transactions on
