Title :
An optimal terminal guidance law
Author :
Nazaroff, Gregory J.
Author_Institution :
Aeronautic Ford, Newport Beach, CA, USA
fDate :
6/1/1976 12:00:00 AM
Abstract :
An optimal terminal guidance law is derived using linear optimal control theory.
Keywords :
Interception problems; Linear systems, time-varying continuous-time; Missile guidance; Optimal control; Acceleration; Aerodynamics; Automatic control; Computer vision; Differential equations; Geometry; Missiles; Optimal control; Proportional control; State estimation;
Journal_Title :
Automatic Control, IEEE Transactions on
DOI :
10.1109/TAC.1976.1101212
