Title :
Discrete Advanced Guidance for High Order Acceleration Constrained Missile
Author_Institution :
Drexel University, ECE dept., Philadelphia, PA 19104.
Abstract :
An explicit closed form formula of a discrete guidance law for a linear, time-invariant, high-order and acceleration-constrained missile is presented. The formula is given in terms of the missile transfer function and acceleration constraint, and responses to initial conditions.
Keywords :
Acceleration; Aerodynamics; Equations; Gold; Missiles; Rockets; Tellurium;
Conference_Titel :
American Control Conference, 1991
Conference_Location :
Boston, MA, USA
Print_ISBN :
0-87942-565-2
