Title :
Linearized kappa guidance
Author :
Serakos, Demetrios ; Lin, Ching-Fang
Author_Institution :
Naval Surface Warfare Center, Dahlgren, VA, USA
fDate :
29 June-1 July 1994
Abstract :
The κ-guidance dynamical equations, which are nonlinear and vary with respect to the independent parameter, range, are linearized and then the LQR method is used to solve the optimal control problem. The linearization is via a nonlinear coordinate transformation and nonlinear feedback. The cost function is approximated by a quadratic cost.
Keywords :
feedback; linear quadratic control; linearisation techniques; military systems; nonlinear control systems; κ-guidance dynamical equations; LQR method; linearized kappa guidance; nonlinear coordinate transformation; nonlinear feedback; optimal control problem; quadratic cost; Adaptive control; Closed loop systems; Cost function; Feedback loop; Nonlinear equations; Optimal control; State feedback;
Conference_Titel :
American Control Conference, 1994
Print_ISBN :
0-7803-1783-1
DOI :
10.1109/ACC.1994.735184
