DocumentCode :
486735
Title :
Multivariable Adaptive Control of a Missile using MAC & CVA
Author :
Mahmood, Shahjahan ; Larimore, Wallace E.
Author_Institution :
Scientific Systems, Inc., Cambridge, MA 02140
fYear :
1986
fDate :
18-20 June 1986
Firstpage :
1482
Lastpage :
1489
Abstract :
Model Algorithmic Control (MAC) is a relatively new control technique which has been applied to many industrial processes during the last few years. Simplified analysis of the technique has shown that MAC, as an output based controller, has excellent robustness properties. It uses a model of the actual plant to compute an optimal control sequence by using an on-line optimization scheme. When the model is not known apriori, a relatively new technique based on Canonical Variate Analysis (CVA) can be used to identify the plant on-line. CVA, using Akaike Information Criteria (AIC), can determine the state-order and can identify a plant or a part of it in a closed loop configuration. It does not need any initialization and yet performs near maximum likelihood. In this paper, MAC and CVA has been integrated together to form an excellent robust adaptive controller known as AMAC (Adaptive MAC). The performance of AMAC has been demonstrated on an air-to-air missile model with asymmetric aerodynamic properties.
Keywords :
Adaptive control; Aerodynamics; Aerospace control; Delay; Electrical equipment industry; Missiles; Open loop systems; Programmable control; Robust control; Testing;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
American Control Conference, 1986
Conference_Location :
Seattle, WA, USA
Type :
conf
Filename :
4789161
Link To Document :
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