Wind Tunnel Tests and Open-Loop Trajectory Simulations for a 155 mm Canards Guided Spin Stabilized Projectile-Reference-Cited by-同舟云学术

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

Published:2008-06-15 Issue: Volume: Page:
ISSN:
Container-title:AIAA Atmospheric Flight Mechanics Conference and Exhibit
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Author:

Wernert Philippe¹,Leopold Friedrich¹,Lehmann Lutz²,Baer Klaus²,Reindler Albrecht²,Bidino Denis³,Juncker Joseph¹

Affiliation:

1. French-German Research Institute of Saint-Louis

2. Diehl BGT Defence GmbH and Company KG

3. French-German Research Institute of Saint Louis

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2008-6881

Reference11 articles.

1. Instability of Spinning Projectiles During Terminal Guidance

2. 5Wernert P. "Simulations de trajectoires de projectiles à six degrés de liberté dans le cadre de la mécanique du vol avion. Partie3: Utilisation derepères nonliés auprojectile",ISL R124/2007, 2007.

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