Fuzzy guidance law for surface-to-air missile in the command control systems

2012 ◽  
Author(s):  
Trung-Dung Pham ◽  
Qui Tran ◽  
Duc-Vuong Vu
Keyword(s):  
Control Systems ◽  
Guidance Law

Robust partial control design for non-linear control systems: a guidance application

2011 ◽  
Vol 226 (2) ◽  
pp. 233-242 ◽  
Author(s):  
T Binazadeh ◽  
M-J Yazdanpanah
Keyword(s):  
Control Systems ◽  
Input Vector ◽  
Guidance System ◽  
Linear Control Systems ◽  
Missile Guidance ◽  
Partial Control ◽  
New Approach ◽  
Guidance Law ◽  
Non Linear ◽  
Guidance Problem

In this paper, a general approach for robust partial stabilization of uncertain non-linear systems is presented. In this approach, the non-linear dynamic system is divided into two subsystems, called the first and the second subsystems. This division is done based on the required stability properties of the system’s states. The reduced input vector (the vector that includes components of the input vector appearing in the first subsystem) is designed to asymptotically stabilize the first subsystem. The proposed scheme is then applied for designing a guidance law as a potential application. Indeed, the paper presents a new approach to the missile guidance problem and shows that asymptotic stability behaviour is not realistic for all states of the guidance system. The effectiveness of the proposed guidance law in interception of manoeuvring targets is demonstrated analytically and through computer simulations.

The amplitude transition function and the manual and oculomotor control systems.

1988 ◽  
Vol 104 (3) ◽  
pp. 363-372 ◽  
Author(s):  
Nicholas C. Barrett ◽  
Denis J. Glencross
Keyword(s):  
Control Systems ◽  
Transition Function ◽  
Oculomotor Control
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