NDLI: Guidance laws in defense against missile attack

Content Provider	IEEE Xplore Digital Library
Author	Rusnak, I.
Copyright Year	2008
Description	Author affiliation: RAFAEL, Haifa, Israel (Rusnak, I.)
Abstract	In defense against missile attack there are three participants. The Target, the Missile, that intercepts the Target, and the Defender, that protects the Target by interception of the missile. This is a three person game, the Target, the Missile and the Defender (TMD) game. The dynamic game theory is applied to derive guidance laws for the TMD scenario. In such scenario the objective of the Defender is minimizing its distance to the Missile while the objective of the Missile is to maximize its distance from the Defender and at the same time not to jeopardize its effort to intercept the Target, i.e. minimizing its miss while the Target performs avoidance maneuvers. The performance of the games theory based guidance law is compared to case when the target performs evasive constant acceleration maneuver, and the missile and defender implement Proportional Navigation. It is shown that the application of the game theory based guidance law reduces significantly the miss of both the target- missile miss and the missile-defender miss as well as the required acceleration levels.
Starting Page	090
Ending Page	094
File Size	438117
Page Count	5
File Format	PDF
ISBN	9781424424818
DOI	10.1109/EEEI.2008.4736664
Language	English
Publisher	Institute of Electrical and Electronics Engineers, Inc. (IEEE)
Publisher Date	2008-12-03
Publisher Place	Israel
Access Restriction	Subscribed
Rights Holder	Institute of Electrical and Electronics Engineers, Inc. (IEEE)
Subject Keyword	Missiles Game theory Acceleration Navigation Protection Information analysis Nash equilibrium Continuous time systems Sufficient conditions Linear systems
Content Type	Text
Resource Type	Article

Sl.	Authority	Responsibilities	Communication Details
1	Ministry of Education (GoI), Department of Higher Education	Sanctioning Authority	https://www.education.gov.in/ict-initiatives
2	Indian Institute of Technology Kharagpur	Host Institute of the Project: The host institute of the project is responsible for providing infrastructure support and hosting the project	https://www.iitkgp.ac.in
3	National Digital Library of India Office, Indian Institute of Technology Kharagpur	The administrative and infrastructural headquarters of the project	Dr. B. Sutradhar bsutra@ndl.gov.in
4	Project PI / Joint PI	Principal Investigator and Joint Principal Investigators of the project	Dr. B. Sutradhar bsutra@ndl.gov.in Prof. Saswat Chakrabarti will be added soon
5	Website/Portal (Helpdesk)	Queries regarding NDLI and its services	support@ndl.gov.in
6	Contents and Copyright Issues	Queries related to content curation and copyright issues	content@ndl.gov.in
7	National Digital Library of India Club (NDLI Club)	Queries related to NDLI Club formation, support, user awareness program, seminar/symposium, collaboration, social media, promotion, and outreach	clubsupport@ndl.gov.in
8	Digital Preservation Centre (DPC)	Assistance with digitizing and archiving copyright-free printed books	dpc@ndl.gov.in
9	IDR Setup or Support	Queries related to establishment and support of Institutional Digital Repository (IDR) and IDR workshops	idr@ndl.gov.in

Games based guidance in anti Missile defence for high order participants

L/sub 2/ stability and performance analysis of missile systems with linear autopilots and PN guidance laws

Distributed multi-missile salvo attack

Two robust homing missile guidance laws based on sliding mode control theory

Improvement of guidance law for simultaneous attack

Game optimal receding horizon guidance laws and its equivalence to receding horizon guidance laws

Pure proportional navigation against time-varying target manoeuvres

Absolute Stability Margin in Missile Guidance Loop

Guidance laws based on Lyapunov theory and DOB for three-dimensional missile-target interception

Guidance laws in defense against missile attack

Similar Documents

Games based guidance in anti Missile defence for high order participants

L/sub 2/ stability and performance analysis of missile systems with linear autopilots and PN guidance laws

Distributed multi-missile salvo attack

Two robust homing missile guidance laws based on sliding mode control theory

Improvement of guidance law for simultaneous attack

Game optimal receding horizon guidance laws and its equivalence to receding horizon guidance laws

Pure proportional navigation against time-varying target manoeuvres

Absolute Stability Margin in Missile Guidance Loop

Guidance laws based on Lyapunov theory and DOB for three-dimensional missile-target interception

Guidance laws in defense against missile attack