Flight Dynamics Properties of 155 mm Spin-Stabilized Projectiles Analyzed in Different Body Frames-Reference-Cited by-同舟云学术

Flight Dynamics Properties of 155 mm Spin-Stabilized Projectiles Analyzed in Different Body Frames

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

Wernert Philippe¹,Theodoulis Spilios¹,Morel Yannick¹

Affiliation:

1. French-German Research Institute of Saint-Louis

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2010-7640

Reference12 articles.

1. Wind Tunnel Tests and Open-Loop Trajectory Simulations for a 155 mm Canards Guided Spin Stabilized Projectile

2. Stability Analysis for Canard Guided Dual-Spin Stabilized Projectiles

3. LPV modeling of guided projectiles for terminal guidance

4. 6Wernert P. "Simulations de trajectoires de projectiles à six degrés de liberté dans le cadre de la mécanique du vol avion. Partie1:Miseen équation et résolutionparla méthodedes quaternions", ISLReportR 123/2004,2004.

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