Please use this identifier to cite or link to this item: https://doi.org/10.1109/CYBER.2013.6705452
Title: The autopilot design of bank-to-turn missile using mixed sensitivity H ∞ optimization
Authors: Luo, D.
Chen, B.M. 
Keywords: autopilot design
bank-to-turn missile
mixed sensitivity H∞ optimization
target interception
Issue Date: 2013
Source: Luo, D.,Chen, B.M. (2013). The autopilot design of bank-to-turn missile using mixed sensitivity H ∞ optimization. 2013 IEEE International Conference on Cyber Technology in Automation, Control and Intelligent Systems, IEEE-CYBER 2013 : 241-246. ScholarBank@NUS Repository. https://doi.org/10.1109/CYBER.2013.6705452
Abstract: Bank-to-turn (BTT) missile shows many advantages in performance over traditional skid-to-turn missile, while the autopilot design poses a great challenge for BTT missile because it is a multivariable system with motion, inertia, aerodynamic and control couplings. In this paper, the autopilot for BTT missile is designed as a two-loop feedback control structure. The inner loop feedback controller is designed using LQR control approach to contain the system uncertainty within a certain limit. The outer loop controller is designed using mixed sensitivity H∞ optimization to deal with the disturbance and model uncertainty. Then simulation experiments of target interception are performed using BTT missile with the designed autopilot under six degrees of freedom. The results demonstrate that the designed autopilot for BTT missile is effective. © 2013 IEEE.
Source Title: 2013 IEEE International Conference on Cyber Technology in Automation, Control and Intelligent Systems, IEEE-CYBER 2013
URI: http://scholarbank.nus.edu.sg/handle/10635/84280
ISBN: 9781479906109
DOI: 10.1109/CYBER.2013.6705452
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