DocumentCode
2544263
Title
Meeting the challenges of modern interceptor guidance by non-conventional approaches
Author
Shinar, Josef ; Turetsky, Vladimir
Author_Institution
Fac. of Aerosp. Eng., Technion - Israel Inst. of Technol., Haifa, Israel
fYear
2009
fDate
24-26 June 2009
Firstpage
1563
Lastpage
1568
Abstract
The challenge of intercepting threats with non conventional warheads, the major drive for the development of ballistic missile defense systems since the first Gulf War of 1991, became even more serious when the reentry vehicles were assumed to be capable of maneuvering. Successful interception of such targets, requiring very small miss distances, cannot be guaranteed by the classical guidance and estimation methods that have been used against manned aircraft. Future interceptor guidance strategy has to be based on pursuit-evasion game concepts and the estimator design has to be integrated with the guidance law. Following such non conventional approaches has the potential to achieve the requirement of hit-to-kill accuracy against randomly maneuvering threats.
Keywords
aircraft control; ballistics; estimation theory; missile guidance; ballistic missile defense systems; estimation methods; estimator design; guidance law; hit-to-kill accuracy; interceptor guidance strategy; manned aircraft; modern interceptor guidance; nonconventional approaches; nonconventional warheads; pursuit-evasion game concepts; reentry vehicles; target interception; Acceleration; Accelerometers; Aerospace engineering; Aircraft; Automatic control; Geometry; Missiles; Navigation; Noise measurement; Optimal control; integrated estimation/guidance; interception; random target maneuver;
fLanguage
English
Publisher
ieee
Conference_Titel
Control and Automation, 2009. MED '09. 17th Mediterranean Conference on
Conference_Location
Thessaloniki
Print_ISBN
978-1-4244-4684-1
Electronic_ISBN
978-1-4244-4685-8
Type
conf
DOI
10.1109/MED.2009.5164770
Filename
5164770
Link To Document