Aerodynamic Stabilization of a Finless Projectile with Active Nose Deflection-Reference-Cited by-同舟云学术

Aerodynamic Stabilization of a Finless Projectile with Active Nose Deflection

Published:2022-09 Issue:5 Volume:59 Page:1592-1601
ISSN:0022-4650
Container-title:Journal of Spacecraft and Rockets
language:en
Short-container-title:Journal of Spacecraft and Rockets

Author:

Butler Cason N.¹,Costello Mark F.¹,Dickinson Benjamin T.²

Affiliation:

1. Georgia Institute of Technology, Atlanta, Georgia 30332

2. Air Force Research Laboratory, Eglin Air Force Base, Florida 32542

Funder

U.S. Air Force Research Laboratory

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.A35352

Reference12 articles.

1. DahlkeC. W. “The Aerodynamic Characteristics of Wrap-Around Fins at Mach Numbers of 0.3 to 3.0,” Army Missile Research Development and Engineering Lab. Rept. RD-77-4, Redstone Arsenal, AL, Aeroballistics Directorate, 1976, https://apps.dtic.mil/sti/citations/ADA036715.

2. Control Authority of a Projectile Equipped with a Controllable Internal Translating Mass

3. Missile Controlled by Lift and Divert Thrusters Using Nonlinear Dynamic Sliding Manifolds

4. Model Predictive Control of a Direct Fire Projectile Equipped With Canards

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