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Equations of Motion for a Modified Point Mass Trajectory.


AD485869

Publication Date 1966
Personal Author Lieske, R. F.; Reiter, M. L.
Page Count 30
Abstract A modified point mass mathematical model, which incorporates an estimate of the yaw of repose, has been developed to represent the flight of a spin stabilized, dynamically stable, artillery shell. This improved mathematical model has the desirable feature of representing the effects of the significant variables of yaw of repose and axial spin along the trajectory. (Author)
Keywords
  • Spin stabilized ammunition
  • Mathematical models
  • Projectiles
  • Momentum
  • Velocity
  • Coriolis effect
  • Exterior ballistics
  • Equations of motion
  • Yaw
  • Spinning(Motion)
  • Projectile trajectories
  • Vector analysis
  • NTISDODXD
Source Agency
  • Non Paid Delimited ADS
NTIS Subject Category
  • 79A - Ammunition, Explosives, & Pyrotechnics
  • 72 - Mathematical Sciences
Corporate Authors Ballistic Research Labs., Aberdeen Proving Ground, MD.
Document Type Technical Report
NTIS Issue Number 198121
Equations of Motion for a Modified Point Mass Trajectory.
Equations of Motion for a Modified Point Mass Trajectory.
AD485869

  • Spin stabilized ammunition
  • Mathematical models
  • Projectiles
  • Momentum
  • Velocity
  • Coriolis effect
  • Exterior ballistics
  • Equations of motion
  • Yaw
  • Spinning(Motion)
  • Projectile trajectories
  • Vector analysis
  • NTISDODXD
  • Non Paid Delimited ADS
  • 79A - Ammunition, Explosives, & Pyrotechnics
  • 72 - Mathematical Sciences
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