DocumentCode
488809
Title
Discrete Advanced Guidance for High Order Acceleration Constrained Missile
Author
Rusnak, Ilan
Author_Institution
Drexel University, ECE dept., Philadelphia, PA 19104.
fYear
1991
fDate
26-28 June 1991
Firstpage
850
Lastpage
851
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;
fLanguage
English
Publisher
ieee
Conference_Titel
American Control Conference, 1991
Conference_Location
Boston, MA, USA
Print_ISBN
0-87942-565-2
Type
conf
Filename
4791493
Link To Document