DocumentCode :
1692031
Title :
Realistic Missile Modeling for Guidance Applications
Author :
Sobh, Mohamed Ali ; Sheirah, Mohamed A.
Author_Institution :
Dept. of Comput. & Syst., Ain Shams Univ., Cairo
fYear :
2006
Firstpage :
155
Lastpage :
164
Abstract :
In this paper, a general missile modeling is presented. An accurate model for missiles is proposed taking into consideration the rigid body dynamics in 3D space with 6 degrees of freedom. Different coordinate systems, variation of missile mass, aerodynamics, air speed and density, gravity, propulsion system, actuators, measurement and tracking devices are also considered. The full model is implemented and integrated within a simulation environment to facilitate missile guidance design. The developed model is optimized for both high simulation speed and accurate calculations. Other modules are implemented to calculate aerodynamics coefficients, generate random signal, provide both conventional and intelligent control, and represents the missile-target engagement visually. The whole system is successfully used to implement different guidance techniques
Keywords :
Simula; aerodynamics; aerospace simulation; control system CAD; data visualisation; intelligent control; missile guidance; target tracking; 3D space; SimulaWorks; actuators; aerodynamics coefficient calculation; air density; air speed; conventional control; coordinate systems; fuzzy control; gravity; intelligent control; measurement devices; missile guidance design; missile mass; missile simulation; propulsion system; random signal generation; realistic missile modeling; rigid body dynamics; tracking devices; visual missile-target engagement representation; Actuators; Aerodynamics; Coordinate measuring machines; Density measurement; Gravity; Intelligent control; Missiles; Propulsion; Signal generators; Velocity measurement;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Computer Engineering and Systems, The 2006 International Conference on
Conference_Location :
Cairo
Print_ISBN :
1-4244-0271-9
Electronic_ISBN :
1-4244-0272-7
Type :
conf
DOI :
10.1109/ICCES.2006.320441
Filename :
4115501
Link To Document :
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