Prediction of swerving motion of a dual-spin projectile with lateral pulse jets in atmospheric flight.

DOI10.1016/S0895-7177(02)00053-5zbMath1054.70021OpenAlexW2001543377MaRDI QIDQ1609415

R. Smith

Publication date: 15 August 2002

Published in: Mathematical and Computer Modelling (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/s0895-7177(02)00053-5

zbMATH Keywords

impact pointlinear projectile theoryupdate interval

Mathematics Subject Classification ID

Variable mass, rockets (70P05) Control of mechanical systems (70Q05)

Related Items (1)

Swerving orientation of spin-stabilized projectile for fixed-cant canard control input

Cites Work

• Attitude Behavior of a Dual-Spin Spacecraft Composed of Asymmetric Bodies
• Attitude Motion of Asymmetric Dual-Spin Spacecraft
• Effects of energy dissipation on the attitude stability of dual-spinsatellites.

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