Title :
Three dimensional mid-course guidance state equations
Author :
Serakos, Demetrios ; Lin, Ching-Fang
Author_Institution :
Combat Syst. Dept., Naval Surface Warfare Center, Dahlgren, VA, USA
Abstract :
The authors develop the state equations for a three dimensional midcourse guidance scheme based on a generalized Kappa guidance approach to the missile-threat intercept problem. The generalization developed utilizes both curvature and torsion as control inputs. The generalization is accomplished with torsion as the additional control
Keywords :
attitude control; differential equations; missile guidance; generalized Kappa guidance approach; missile-threat intercept problem; three dimensional mid-course guidance state equations; Azimuth; Equations; Interference; Missiles; Sun; Trajectory; Velocity control;
Conference_Titel :
American Control Conference, 1999. Proceedings of the 1999
Conference_Location :
San Diego, CA
Print_ISBN :
0-7803-4990-3
DOI :
10.1109/ACC.1999.786194
