TY - GEN
T1 - Mixed H2/H∞ linear parameter varying state feedback control for bank-to-turn missile autopilot design
AU - Hui, Li
AU - Chengqi, Guan
AU - Danjie, Zhou
AU - Fengyi, Li
AU - Xu, Zha
PY - 2010
Y1 - 2010
N2 - This paper presents a mixed H2/H∞ linear parameter varying state feedback control approach for a bank-to-turn missile autopilot design. A mixed H2/H∞ linear parameter varying state feedback control is proposed firstly. In a polytopic domain, linear matrix inequality conditions that depend only on the vertices of polytope are presented to make sure that the prescribed H2 attenuation level, H∞ attenuation level and the stability of the closed-loop system are guaranteed. Then the pole placement method is combined into the proposed controller design to meet some time response characteristics of the closed-loop system. Therefore, the solution of the gain scheduled controller is obtained. There are no structural constraints on the plant and the presented approach can obtain less conservative results than some previous results. Furthermore, the approach is applied to a bank-to-turn missile pitch-axis autopilot design over full flight envelope, the capability and effectiveness of the proposed approach is demonstrated by the results.
AB - This paper presents a mixed H2/H∞ linear parameter varying state feedback control approach for a bank-to-turn missile autopilot design. A mixed H2/H∞ linear parameter varying state feedback control is proposed firstly. In a polytopic domain, linear matrix inequality conditions that depend only on the vertices of polytope are presented to make sure that the prescribed H2 attenuation level, H∞ attenuation level and the stability of the closed-loop system are guaranteed. Then the pole placement method is combined into the proposed controller design to meet some time response characteristics of the closed-loop system. Therefore, the solution of the gain scheduled controller is obtained. There are no structural constraints on the plant and the presented approach can obtain less conservative results than some previous results. Furthermore, the approach is applied to a bank-to-turn missile pitch-axis autopilot design over full flight envelope, the capability and effectiveness of the proposed approach is demonstrated by the results.
KW - Autopilot design
KW - Bank-to-turn missile
KW - Linear parameter varying systems
KW - Mixed H/H state feedback control
UR - http://www.scopus.com/inward/record.url?scp=78649995158&partnerID=8YFLogxK
U2 - 10.1109/CMCE.2010.5610481
DO - 10.1109/CMCE.2010.5610481
M3 - Conference contribution
AN - SCOPUS:78649995158
SN - 9781424479566
T3 - 2010 International Conference on Computer, Mechatronics, Control and Electronic Engineering, CMCE 2010
SP - 240
EP - 246
BT - 2010 International Conference on Computer, Mechatronics, Control and Electronic Engineering, CMCE 2010
T2 - 2010 International Conference on Computer, Mechatronics, Control and Electronic Engineering, CMCE 2010
Y2 - 24 August 2010 through 26 August 2010
ER -