DocumentCode
3070043
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
Volume
6
fYear
1999
fDate
1999
Firstpage
3738
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;
fLanguage
English
Publisher
ieee
Conference_Titel
American Control Conference, 1999. Proceedings of the 1999
Conference_Location
San Diego, CA
ISSN
0743-1619
Print_ISBN
0-7803-4990-3
Type
conf
DOI
10.1109/ACC.1999.786194
Filename
786194
Link To Document