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Accession Number ADA584825
Title Integrated Navigation, Guidance, and Control of Missile Systems: 3-D Dynamic Model.
Publication Date Feb 2013
Media Count 36p
Personal Author F. A. Faruqi
Abstract In this report a 3-D mathematical modelfor multi-party engagement kinematics is derived suitable for developing, implementing and testing modern missile guidance systems. The model developed here is suitable for both conventional and more advanced optimal intelligent guidance schemes including those that arise out of the differential game theory. This model accommodates changes in vehicle body attitude and other non-linear effects such as limits on lateral acceleration and aerodynamic forces.
Keywords Aerodynamic forces
Australia
Control
Foreign reports
Game theory
Guided missiles
Integrated systems
Kinematics
Mathematical models
Navigation
Nonlinear systems
Three dimensional
Weapon systems


 
Source Agency Non Paid ADAS
NTIS Subject Category 75 - Missile Technology
79F - Fire Control & Bombing Systems
Corporate Author Defence Science and Technology Organisation, Canberra (Australia). Weapons System Div.
Document Type Technical report
Title Note Technical rept.
NTIS Issue Number 1403
Contract Number N/A

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