Predicting the Flight Behaviour of a Guided Projectile Through a Six Degrees of Freedom Trajectory Model
Author:
Publisher
Springer Nature Singapore
Link
https://link.springer.com/content/pdf/10.1007/978-981-99-5755-2_49
Reference8 articles.
1. Fowler R, Gallop E, Lock C, Richmond H (1920) The aerodynamics of spinning shell. Philos Trans Roy Soc Lond Ser A: Math Phys Sci 221:199–205
2. Cooper G (2001) Influence of yaw cards on the yaw growth of spin stabilized projectiles. J Aircr 38(2):266–270
3. Guidos B, Cooper G (2000) Closed form solution of finned projectile motion subjected to a simple in-flight lateral impulse. AIAA Paper 2000-0767
4. Gkritzapis D, Panagiotopoulos E (2009) Accurate computation of the trajectory of the spin and fin-stabilized projectiles. Int J Math Comput Simul 3(2):73–80
5. Gkritzapis D, Panagiotopoulos E, Margaris D, Papanikas D (2007) A six degree of freedom trajectory analysis of spin-stabilized projectiles. AIP Conf Proc 963:1187
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