Title :
Pure proportional navigation against time-varying target manoeuvres
Author :
Ghawghawe, S.N. ; Ghose, D.
Author_Institution :
Dept. of Aerosp. Eng., Indian Inst. of Sci., Bangalore, India
fDate :
10/1/1996 12:00:00 AM
Abstract :
Capturability of the pure proportional navigation (PPN) guidance law against a target executing bounded piecewise continuous time-varying manoeuvres is investigated. A qualitative analysis is carried out to obtain a set of sufficient conditions for capture defined on the engagement parameters and initial conditions. These conditions are significantly less restrictive than the ones obtained previously by others using the Lyapunov method. It is shown that the actual capture region for time-varying target manoeuvres, obtained by using the conditions derived, is much larger than that obtained from the Lyapunov technique. We also show that though a bounded tine varying target manoeuvre does change the constant target manoeuvre capture region to some extent, it does not reduce it drastically. Further, we show that the worst case capture region is obtained when the target executes a constant manoeuvre equal to the bound on the manoeuvre level. Some bounds on the missile lateral acceleration are also obtained for certain regions in the engagement plane. These results are generalizations and extensions of existing results on the capturability of the PPN guidance law against targets executing constant or time-varying target manoeuvres
Keywords :
missile guidance; optimal control; target tracking; time-varying systems; Lyapunov method; constant target manoeuvre capture region; engagement parameters; guidance law; missile lateral acceleration; piloted aircraft target; pure proportional navigation; qualitative analysis; sufficient conditions; target executing bounded piecewise continuous time-varying manoeuvres; time-varying target manoeuvres; worst case capture region; Acceleration; Aircraft; Closed-form solution; Game theory; Geometry; Information systems; Missiles; Navigation; Optimal control; Sufficient conditions;
Journal_Title :
Aerospace and Electronic Systems, IEEE Transactions on