Modeling and Vertical Launch Analysis of an Aero- and Thrust Vector Controlled Surface to Air Missile-Reference-Cited by-同舟云学术

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Modeling and Vertical Launch Analysis of an Aero- and Thrust Vector Controlled Surface to Air Missile

Published:2010-06-14 Issue: Volume: Page:
ISSN:
Container-title:AIAA Atmospheric Flight Mechanics Conference
language:
Short-container-title:

Author:

Tekin Raziye¹,Atesoglu Özgür²,Leblebicioglu Kemal²

Affiliation:

1. Roketsan Missiles, Inc.

2. Middle East Technical University

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2010-7639

Reference21 articles.

1. Solis,R."AnAnalysisoftheVerticalLaunchPhaseofaMissileConcept,"AIAAAerospaceSciencesMeeting,1983.

2. 2Woodberry,R.F.H.,andZeamer,R.J."SolidRocketThrustVectorControl,",NASA-SP-8114,1974.

3. Evolved SeaSparrow Missile Jet Vane Control System Prototype Hardware Development

4. U.S.StandardAtmosphere,U.S.GovernmentPrintingOffice,Washington,D.C.,1976.

5. Atesoglu, Ö. "High Alpha Maneuvering and Stabilization Control of Flight Vehicles," Ph.D. Dissertation,Mechanical Engineering Dept., METU,2007.

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