3550547

Design of a missile autopilot using adaptive nonlinear dynamic inversion

Hindman, Rick ; Shell, William M.

Raytheon Missile Syst., Tucson, AZ, USA

2005

June 8-10, 2005

327

332

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;

English

ieee

American Control Conference, 2005. Proceedings of the 2005

0743-1619

0-7803-9098-9

0743-1619

conf

10.1109/ACC.2005.1469954

1469954