An Approximate Method to Calculate Nonlinear Rolling Moment Due to Differential Fin Deflection

Moore, Frankie; Moore, Linda Y.

doi:10.2514/6.2012-692

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2013

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“…A canted fin-stabilized, canard-controlled projectile flying in a skid-to-turn configuration was selected based on past work (19), which complicates the aerodynamic characterization resulting from flow interactions (18,20,21). Packaging constraints for gun tube launch require deploying stabilizing and control surfaces.…”

Section: Introductionmentioning

confidence: 99%

Projectile Roll Dynamics and Control With a Low-Cost Skid-to-Turn Maneuver System

Fresconi¹,

Celmins²,

Ilg³

et al. 2013

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