It is shown that the optimal guidance problem can be handled as a Bolza-type problem which can be solved by straightforward calculation. The solution proves to be different from that given by Yang, et al. (1989) and is verified to be a minimum performance index solution. Also presented is an alternate unified approach to the solution of the nonlinear system of differential equation of the generalized proportional navigation law discussed earlier by Yang, et al. This unified equation has been solved for all the different cases of proportional navigation for which closed-form solutions have been published by earlier authors.<>
Analysis of generalized guidance laws for homing missiles
IEEE Transactions on Aerospace and Electronic Systems ; 31 , 2 ; 514-521
1995-04-01
359163 byte
Article (Journal)
Electronic Resource
English
Analysis of Generalized Guidance Laws for Homing Missiles
Online Contents | 1995
|Generalized guidance law for homing missiles
IEEE | 1989
|Generalized guidance law for homing missiles
Tema Archive | 1989
|