A novel guidance law designed specifically for a missile having forward and aft control systems is presented. For the derivation a linear quadratic differential games formulation of the end-game interception scenario is used. Conditions for achieving perfect intercept are given and new game spaces are presented. It is also shown that increasing the direct lift associated with the canard control allows intercepting targets with higher maneuvering capability, while for the tail control the effect is opposite.
Linear Quadratic Differential Games Guidance Law for Dual Controlled Missiles
IEEE Transactions on Aerospace and Electronic Systems ; 43 , 3 ; 834-842
2007-07-01
1492268 byte
Article (Journal)
Electronic Resource
English
Linear Quadratic Differential Games Guidance Law for Dual Controlled Missiles
Online Contents | 2007
|AIAA-2002-4841 Linear Quadratic Guidance Laws for Missiles Having Dual Control Systems
British Library Conference Proceedings | 2002
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