DocumentCode :
3550547
Title :
Design of a missile autopilot using adaptive nonlinear dynamic inversion
Author :
Hindman, Rick ; Shell, William M.
Author_Institution :
Raytheon Missile Syst., Tucson, AZ, USA
fYear :
2005
fDate :
June 8-10, 2005
Firstpage :
327
Lastpage :
332
Keywords :
aerodynamics; feedback; interpolation; inverse problems; missile guidance; model reference adaptive control systems; nonlinear dynamical systems; robust control; ANDI autopilot; adaptive element; adaptive nonlinear dynamic inversion; aerodynamic modeling; gain table; gain values; interpolation; missile autopilot; missile flight condition; missile flight envelope; parameter variation; reference model; robustness; stability; three loop feedback topology; Actuators; Aerodynamics; Artificial neural networks; Error correction; Feedback loop; Interpolation; Missiles; Performance gain; Robust stability; Topology;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
American Control Conference, 2005. Proceedings of the 2005
ISSN :
0743-1619
Print_ISBN :
0-7803-9098-9
Electronic_ISBN :
0743-1619
Type :
conf
DOI :
10.1109/ACC.2005.1469954
Filename :
1469954
Link To Document :
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