Flight dynamics of the boomerang, part 2: Effects of initial conditions and geometrical configuration

Journal of Guidance, Control, and Dynamics

Volumn 27, Issue 4, 2004, Pages 555-563

  Beppu, Goro ^a,d   Ishikawa, Hiroaki ^a,d   Azuma, Akira ^b,d   Yasuda, Kunio ^c,d  

^a TOKAI UNIVERSITY   (Japan)

^b UNIVERSITY OF TOKYO   (Japan)

^c NIHON UNIVERSITY   (Japan)

^d Department of Aeronautics ^*

Author keywords

[No Author keywords available]

Indexed keywords

EQUATIONS OF MOTION; GRAVITATIONAL EFFECTS; GYROSCOPES; KINETIC ENERGY; NONLINEAR EQUATIONS; VECTORS;

AERODYNAMIC FORCES; BOOMERANGS; MOMENT OF INERTIA;

FLIGHT DYNAMICS;

EID: 3843116516     PISSN: 07315090     EISSN: 15333884     Source Type: Journal    
DOI: 10.2514/1.11158     Document Type: Article

References (1)

1. Azuma, A., Beppu, G., Ishikawa, H., and Yasuda, K., "Flight Dynamics of the Boomerang, Part 1: Fundamental Analysis," Journal of Guidance, Control, and Dynamics, Vol. 27, No. 4. 2004, pp. 545-554.