We suggest a first-order model to distinguish between nose control (canards) and tail control. We present optimal guidance strategies and demonstrate the superiority of nose control. This simple model enables us to develop simple and robust guidance strategies based on three approaches: unconstrained optimal control, constrained optimal control, and constrained differential games. It turns out that nose control requires low gain and is capable of forcing small miss distance in the presence of a maneuvering target.
Superiority of canards in homing missiles
IEEE Transactions on Aerospace and Electronic Systems ; 39 , 3 ; 740-746
2003-07-01
458123 byte
Article (Journal)
Electronic Resource
English
Superiority of Canards in Homing Missiles
Online Contents | 2003
|Neoclassical Guidance for Homing Missiles
AIAA | 2001
|Optimal Controllers for Homing Missiles
NTIS | 1968
|Hyperstable range in homing missiles
AIAA | 1990
|The development of radar homing missiles
AIAA | 1984
|