Dynamic stability of unguided projectile with 6- DOF trajectory modeling

The paper presents the study of unguided rolling projectiles at varying Mach numbers using aerodynamic coefficients. The aerodynamic coefficients are estimated using an aerodynamic prediction code, Missile DATCOM. The predicted dynamic derivatives will determine the design criteria, and also their...

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Main Authors:	Bashir, Musavir, Khan, Sher Afghan, Udayagiri, Leelanadh, Noor, Asim
Format:	Conference or Workshop Item
Language:	English
Published:	IEEE Explorer 2017
Subjects:	TL Motor vehicles. Aeronautics. Astronautics
Online Access:	http://irep.iium.edu.my/60787/ http://irep.iium.edu.my/60787/ http://irep.iium.edu.my/60787/ http://irep.iium.edu.my/60787/1/08226280.pdf

id	iium-60787
recordtype	eprints
spelling	iium-607872017-12-26T10:15:08Z http://irep.iium.edu.my/60787/ Dynamic stability of unguided projectile with 6- DOF trajectory modeling Bashir, Musavir Khan, Sher Afghan Udayagiri, Leelanadh Noor, Asim TL Motor vehicles. Aeronautics. Astronautics The paper presents the study of unguided rolling projectiles at varying Mach numbers using aerodynamic coefficients. The aerodynamic coefficients are estimated using an aerodynamic prediction code, Missile DATCOM. The predicted dynamic derivatives will determine the design criteria, and also their effect on the design aspects (stability and accuracy) of the projectile. To satisfy the condition of stability for the trajectory of projectile, a model of 6 DOF equations has been used. The result parameters, such as static margin of the projectile, force and moment derivatives in all the three modes, spin rate, angle of attack, and time rate are shown. The accuracy of the rolling moment derivatives is uncertain due to the limitation of DATCOM, but it is the general method applicable at the initial design stage of any projectile and therefore falls in the realm of aerodynamic database. The results address the problems of static and dynamic stability by giving initial perturbations, effect of spin on thrust misalignment, and effect of variation in the geometric parameters during the power on and off cases. Therefore, there is a need for full aerodynamic characterization of the projectile, in which sufficient derivatives are computed for accurate results. IEEE Explorer 2017-12-21 Conference or Workshop Item PeerReviewed application/pdf en http://irep.iium.edu.my/60787/1/08226280.pdf Bashir, Musavir and Khan, Sher Afghan and Udayagiri, Leelanadh and Noor, Asim (2017) Dynamic stability of unguided projectile with 6- DOF trajectory modeling. In: 2017 2nd International Conference for Convergence in Technology (I2CT), 7-9 April 2017, Pune, Maharashtra, India. http://ieeexplore.ieee.org/document/8226280/ DOI: 10.1109/I2CT.2017.8226280
repository_type	Digital Repository
institution_category	Local University
institution	International Islamic University Malaysia
building	IIUM Repository
collection	Online Access
language	English
topic	TL Motor vehicles. Aeronautics. Astronautics
spellingShingle	TL Motor vehicles. Aeronautics. Astronautics Bashir, Musavir Khan, Sher Afghan Udayagiri, Leelanadh Noor, Asim Dynamic stability of unguided projectile with 6- DOF trajectory modeling
description	The paper presents the study of unguided rolling projectiles at varying Mach numbers using aerodynamic coefficients. The aerodynamic coefficients are estimated using an aerodynamic prediction code, Missile DATCOM. The predicted dynamic derivatives will determine the design criteria, and also their effect on the design aspects (stability and accuracy) of the projectile. To satisfy the condition of stability for the trajectory of projectile, a model of 6 DOF equations has been used. The result parameters, such as static margin of the projectile, force and moment derivatives in all the three modes, spin rate, angle of attack, and time rate are shown. The accuracy of the rolling moment derivatives is uncertain due to the limitation of DATCOM, but it is the general method applicable at the initial design stage of any projectile and therefore falls in the realm of aerodynamic database. The results address the problems of static and dynamic stability by giving initial perturbations, effect of spin on thrust misalignment, and effect of variation in the geometric parameters during the power on and off cases. Therefore, there is a need for full aerodynamic characterization of the projectile, in which sufficient derivatives are computed for accurate results.
format	Conference or Workshop Item
author	Bashir, Musavir Khan, Sher Afghan Udayagiri, Leelanadh Noor, Asim
author_facet	Bashir, Musavir Khan, Sher Afghan Udayagiri, Leelanadh Noor, Asim
author_sort	Bashir, Musavir
title	Dynamic stability of unguided projectile with 6- DOF trajectory modeling
title_short	Dynamic stability of unguided projectile with 6- DOF trajectory modeling
title_full	Dynamic stability of unguided projectile with 6- DOF trajectory modeling
title_fullStr	Dynamic stability of unguided projectile with 6- DOF trajectory modeling
title_full_unstemmed	Dynamic stability of unguided projectile with 6- DOF trajectory modeling
title_sort	dynamic stability of unguided projectile with 6- dof trajectory modeling
publisher	IEEE Explorer
publishDate	2017
url	http://irep.iium.edu.my/60787/ http://irep.iium.edu.my/60787/ http://irep.iium.edu.my/60787/ http://irep.iium.edu.my/60787/1/08226280.pdf
first_indexed	2023-09-18T21:26:10Z
last_indexed	2023-09-18T21:26:10Z
_version_	1777412206336409600

Dynamic stability of unguided projectile with 6- DOF trajectory modeling

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