Title :
Dual Control Guidance Law for Homing Missiles
Author_Institution :
Department of Aerospace Engineering and Engineering Mechanics, The University of Texas at Austin
Keywords :
Acceleration; Filters; Goniometers; Mechanical variables measurement; Missiles; Navigation; Performance analysis; State estimation; Testing; Trajectory;
Conference_Titel :
Aerospace Control Systems, 1993. Proceedings. The First IEEE Regional Conference on
DOI :
10.1109/AEROCS.1993.721002
