TY - GEN
T1 - Pole assignment method with state constraints for missile three-loop autopilot design
AU - Chang, Chao
AU - Lin, De Fu
AU - Wang, Jiang
PY - 2009
Y1 - 2009
N2 - The three-loop autopilot is transformed into states space model, and the feasibility of presupposition of some nuisance parameter is proved. A new pole assignment method is studied. Considering the actuator state feedback constraints, search methods are used to find the additional poles introduced by actuator. The design results show that, with the new method, all the poles of the system can be assigned to the desired place.
AB - The three-loop autopilot is transformed into states space model, and the feasibility of presupposition of some nuisance parameter is proved. A new pole assignment method is studied. Considering the actuator state feedback constraints, search methods are used to find the additional poles introduced by actuator. The design results show that, with the new method, all the poles of the system can be assigned to the desired place.
KW - Pole assignment
KW - State feedback constraints
KW - Three-loop autopilot
UR - http://www.scopus.com/inward/record.url?scp=70449394583&partnerID=8YFLogxK
U2 - 10.1109/CCDC.2009.5192835
DO - 10.1109/CCDC.2009.5192835
M3 - Conference contribution
AN - SCOPUS:70449394583
SN - 9781424427239
T3 - 2009 Chinese Control and Decision Conference, CCDC 2009
SP - 3298
EP - 3301
BT - 2009 Chinese Control and Decision Conference, CCDC 2009
T2 - 2009 Chinese Control and Decision Conference, CCDC 2009
Y2 - 17 June 2009 through 19 June 2009
ER -